Polyethylene composition and film having a good permeability, stiffness and sealability

ABSTRACT

A polyethylene composition includes a first polyethylene which is an ethylene copolymer having a weight average molecular weight of from 70,000 to 250,000 and a molecular weight distribution Mw/Mn of &lt;2.3, a second polyethylene which is an ethylene copolymer or homopolymer having a weight average molecular weight of from 15,000 to 100,000 and a molecular weight distribution Mw/Mn of &lt;2.3, and a third polyethylene which is an ethylene copolymer or homopolymer having a weight average molecular weight of from 70,000 to 250,000 and a molecular weight distribution Mw/Mn of &gt;2.3, where the first polyethylene has more short chain branching than the second polyethylene or the third polyethylene. The polyethylene composition has a soluble fraction in a CEF analysis of at least 10 weight percent. Film made from the polyethylene composition may have a machine direction 1% secant modulus of ≥190 MPa (at a film thickness of about 1 mil), a seal initiation temperature (SIT) of ≤100° C. (at a film thickness of about 2 mil), an area of hot tack window (AHTW) of ≥160 Newtons·C° (at a film thickness of about 2 mil) and an oxygen transmission rate (OTR) of ≥650 cm3 per 100 inch2 (at a film thickness of about 1 mil).

This application claims the benefit of the earlier filing date ofCanadian Application Serial Number 3011038 filed on Jul. 11, 2018, whichapplication is incorporated herein by reference in its entirety.

The present disclosure provides polyethylene compositions which whenblown into film have good stiffness, good oxygen permeability and goodsealability. The polyethylene compositions include two polyethylenecomponents which are made with a single site polymerization catalyst andone polyethylene component which is made with multi-site polymerizationcatalysts.

Multicomponent polyethylene compositions are well known in the art. Onemethod to access multicomponent polyethylene compositions is to use twoor more distinct polymerization catalysts in one or more polymerizationreactors. For example, the use of single site and Ziegler-Natta typepolymerization catalysts in at least two distinct solutionpolymerization reactors is known. Such reactors may be configured inseries or in parallel.

Solution polymerization processes are generally carried out attemperatures above the melting point of the ethylene homopolymer orcopolymer product being made. In a typical solution polymerizationprocess, catalyst components, solvent, monomers and hydrogen are fedunder pressure to one or more reactors.

For solution phase ethylene polymerization, or ethylenecopolymerization, reactor temperatures can range from about 80° C. toabout 300° C. while pressures generally range from about 3 MPag to about45 MPag. The ethylene homopolymer or copolymer produced remainsdissolved in the solvent under reactor conditions. The residence time ofthe solvent in the reactor is relatively short, for example, from about1 second to about 20 minutes. The solution process can be operated undera wide range of process conditions that allow the production of a widevariety of ethylene polymers. Post reactor, the polymerization reactionis quenched to prevent further polymerization, by adding a catalystdeactivator, and optionally passivated, by adding an acid scavenger.Once deactivated (and optionally passivated), the polymer solution ispassed to a polymer recovery operation (a devolatilization system) wherethe ethylene homopolymer or copolymer is separated from process solvent,unreacted residual ethylene and unreacted optional α-olefin(s).

Regardless of the manner of production, there remains a need to improvethe performance of multicomponent polyethylene compositions in filmapplications.

The present disclosure provides polyethylene compositions which whenmade into film have a good balance of stiffness, oxygen transmissionrates, and sealing properties.

An embodiment of the disclosure is a polyethylene composition including:

from 5 to 80 wt. % of a first polyethylene which is an ethylenecopolymer, the first polyethylene having a weight average molecularweight M_(W) of from 70,000 to 250,000, a molecular weight distributionM_(w)/M_(n) of <2.3 and from 5 to 100 short chain branches per thousandcarbon atoms;

from 5 to 80 wt. % of a second polyethylene which is an ethylenecopolymer or an ethylene homopolymer, the second polyethylene having aweight average molecular weight M_(W) of from 15,000 to 100,000, amolecular weight distribution M_(w)/M_(n) of <2.3 and from 0 to 20 shortchain branches per thousand carbon atoms; and

from 5 to 80 wt. % of a third polyethylene which is an ethylenecopolymer or an ethylene homopolymer, the third polyethylene having aweight average molecular weight M_(W) of from 70,000 to 250,000, amolecular weight distribution M_(w)/M_(n) of >2.3 and from 0 to 50 shortchain branches per thousand carbon atoms; wherein

the number of short chain branches per thousand carbon atoms in thefirst polyethylene (SCB_(PE-1)) is greater than the number of shortchain branches per thousand carbon atoms in the second polyethylene(SCB_(PE-2)) and the third polyethylene (SCB_(PE-3));

the number of short chain branches per thousand carbon atoms in thethird polyethylene (SCB_(PE-3)) is greater than the number of shortchain branches per thousand carbon atoms in the second polyethylene(SCB_(PE-2)); and

the weight average molecular weight of the second polyethylene is lessthan the weight average molecular weight of the first polyethylene andthe third polyethylene; wherein,

the polyethylene composition has a density of ≤0.939 g/cm³, a melt indexI₂ of from 0.1 to 10 dg/min, a melt flow ratio, I₂₁/I₂ of ≤40 and has asoluble fraction in a crystallization elution fractionation (CEF)analysis of at least 10 weight percent.

An embodiment of the disclosure is a film layer having a thickness offrom 0.5 to 10 mil, including a polyethylene composition including:

from 5 to 80 wt. % of a first polyethylene which is an ethylenecopolymer, the first polyethylene having a weight average molecularweight M_(W) of from 70,000 to 250,000, a molecular weight distributionM_(w)/M_(n) of <2.3 and from 5 to 100 short chain branches per thousandcarbon atoms;

from 5 to 80 wt. % of a second polyethylene which is an ethylenecopolymer or an ethylene homopolymer, the second polyethylene having aweight average molecular weight M_(W) of from 15,000 to 100,000, amolecular weight distribution M_(w)/M_(n) of <2.3 and from 0 to 20 shortchain branches per thousand carbon atoms; and

from 5 to 80 wt. % of a third polyethylene which is an ethylenecopolymer or an ethylene homopolymer, the third polyethylene having aweight average molecular weight M_(W) of from 70,000 to 250,000, amolecular weight distribution M_(w)/M_(n) of >2.3 and from 0 to 50 shortchain branches per thousand carbon atoms; wherein

the number of short chain branches per thousand carbon atoms in thefirst polyethylene (SCB_(PE-1)) is greater than the number of shortchain branches per thousand carbon atoms in the second polyethylene(SCB_(PE-2)) and the third polyethylene (SCB_(PE-3));

the number of short chain branches per thousand carbon atoms in thethird polyethylene (SCB_(PE-3)) is greater than the number of shortchain branches per thousand carbon atoms in the second polyethylene(SCB_(PE-2)); and

the weight average molecular weight of the second polyethylene is lessthan the weight average molecular weight of the first polyethylene andthe third polyethylene; wherein,

the polyethylene composition has a density of ≤0.939 g/cm³, a melt indexI₂ of from 0.1 to 10 dg/min, a melt flow ratio, I₂₁/I₂ of ≤40 and has asoluble fraction in a crystallization elution fractionation (CEF)analysis of at least 10 weight percent.

In an embodiment, a film layer has a machine direction (MD) 1% secantmodulus of ≥190 MPa when measured at a film thickness of about 1 mil.

In an embodiment, a film layer has a seal initiation temperature (SIT)of ≤100° C. when measured at a film thickness of about 2 mil.

In an embodiment, a film layer has an area of hot tack window (AHTW) of≥160 Newtons·° C. when measured at a film thickness of about 2 mil.

In an embodiment, a film layer has an oxygen transmission rate (OTR) of≥650 cm³ per 100 inch² when measured at a film thickness of about 1 mil.

An embodiment of the disclosure, is a film layer having a thickness offrom 0.5 to 10 mil, wherein the film layer has a has a machine direction(MD) 1% secant modulus of ≤190 MPa when measured at a film thickness ofabout 1 mil, an oxygen transmission rate (OTR) of ≥650 cm³ per 100 inch²when measured at a film thickness of about 1 mil, a seal initiationtemperature (SIT) of ≤100° C. when measured at a film thickness of about2 mil, and an area of hot tack window (AHTW) of ≥160 Newtons·° C. whenmeasured at a film thickness of about 2 mil.

An embodiment of the disclosure is a film layer having a thickness offrom 0.5 to 10 mil, wherein the film layer satisfies at least one of thefollowing relationships:

i) area of hot tack window (AHTW)>−2.0981 (machine direction (MD) 1%secant modulus)+564.28;

wherein the AHTW is measured at a film thickness of about 2 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil;

ii) oxygen transmission rate (OTR)>−5.4297 (machine direction (MD) 1%secant modulus)+1767.8;

wherein the OTR is measured at a film thickness of about 1 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil; and

iii) seal initiation temperature (SIT)<0.366 (machine direction (MD) 1%secant modulus)+22.509;

wherein the SIT is measured at a film thickness of about 2 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil.

An embodiment of the disclosure is a film layer having a thickness offrom 0.5 to 10 mil, wherein the film layer satisfies each of thefollowing relationships:

i) area of hot tack window (AHTW)>−2.0981 (machine direction (MD) 1%secant modulus)+564.28;

wherein the AHTW is measured at a film thickness of about 2 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil;

ii) oxygen transmission rate (OTR)>−5.4297 (machine direction (MD) 1%secant modulus)+1767.8;

wherein the OTR is measured at a film thickness of about 1 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil; and

iii) seal initiation temperature (SIT)<0.366 (machine direction (MD) 1%secant modulus)+22.509;

wherein the SIT is measured at a film thickness of about 2 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1 shows the gel permeation chromatographs (GPC) with refractiveindex detection of polyethylene compositions made according to thepresent disclosure as well as for some comparative polyethylenes.

FIG. 2 shows the gel permeation chromatographs with Fourier transforminfra-red (GPC-FTIR) detection obtained for polyethylene compositionsmade according to the present disclosure as well as for some comparativepolyethylenes. The comonomer content, shown as the number of short chainbranches per 1000 carbons (y-axis), is given relative to the copolymermolecular weight (x-axis). The upwardly sloping line (from left toright) is the short chain branching (in short chain branches per 1000carbons atoms) determined by FTIR. As can be seen in the Figure, forInventive Examples 1 and 2, the number of short chain branches initiallyincreases at higher molecular weights and then decreases again at stillhigher molecular weights, and hence the comonomer incorporation is saidto be “partially reversed” with a peak or maximum present.

FIG. 3 shows the differential scanning calorimetry analysis (DSC) andprofile of polyethylene compositions made according to the presentdisclosure as well as for some comparative polyethylenes.

FIG. 4 shows the hot tack profiles for films made using the polyethylenecompositions made according to the present disclosure as well as thosefor several comparative polyethylenes.

FIG. 5 shows the cold seal profiles for films made using thepolyethylene compositions made according to the present disclosure aswell as those for several comparative polyethylenes.

FIG. 6 shows a plot of the equation: AHTW=−2.0981 (machine direction(MD) 1% secant modulus)+564.28. The values for the AHTW (the y-axis) areplotted against the corresponding machine direction (MD) 1% secantmodulus values (the x-axis) for films made from the polyethylenecompositions of the present disclosure as well as those for films madefrom several comparative polyethylenes.

FIG. 7 shows a plot of the equation: SIT=0.366 (machine direction (MD)1% secant modulus)+22.509. The values for the SIT (the y-axis) areplotted against the corresponding machine direction (MD) 1% secantmodulus values (the x-axis) for films made from the polyethylenecompositions of the present disclosure as well as those for films madefrom several comparative polyethylenes.

FIG. 8 shows a plot of the equation: OTR=−5.4297 (machine direction (MD)1% secant modulus)+1767.8. The values for the OTR (the y-axis) areplotted against the corresponding machine direction (MD) 1% secantmodulus values (the x-axis) for films made from the polyethylenecompositions of the present disclosure as well as those for films madefrom several comparative polyethylenes. “1/2.5 film” means that the filmwas made at 1 mil of thickness with a blow up ratio (BUR) of 2.5.

DEFINITION OF TERMS

Other than in the examples or where otherwise indicated, all numbers orexpressions referring to quantities of ingredients, extrusionconditions, etc., used in the specification and claims are to beunderstood as modified in all instances by the term “about.”Accordingly, unless indicated to the contrary, the numerical parametersset forth in the following specification and attached claims areapproximations that can vary depending upon the desired properties thatthe various embodiments desire to obtain. At the very least, and not asan attempt to limit the application of the doctrine of equivalents tothe scope of the claims, each numerical parameter should at least beconstrued in light of the number of reported significant digits and byapplying ordinary rounding techniques. The numerical values set forth inthe specific examples are reported as precisely as possible. Anynumerical values, however, inherently contain certain errors necessarilyresulting from the standard deviation found in their respective testingmeasurements.

It should be understood that any numerical range recited herein isintended to include all sub-ranges subsumed therein. For example, arange of “1 to 10” is intended to include all sub-ranges between andincluding the recited minimum value of 1 and the recited maximum valueof 10; that is, having a minimum value equal to or greater than 1 and amaximum value of equal to or less than 10. Because the disclosednumerical ranges are continuous, they include every value between theminimum and maximum values. Unless expressly indicated otherwise, thevarious numerical ranges specified in this application areapproximations.

All compositional ranges expressed herein are limited in total to and donot exceed 100 percent (volume percent or weight percent) in practice.Where multiple components can be present in a composition, the sum ofthe maximum amounts of each component can exceed 100 percent, with theunderstanding that, and as those skilled in the art readily understand,that the amounts of the components actually used will conform to themaximum of 100 percent.

In order to form a more complete understanding of this disclosure thefollowing terms are defined and should be used with the accompanyingfigures and the description of the various embodiments throughout.

As used herein, the term “monomer” refers to a small molecule that maychemically react and become chemically bonded with itself or othermonomers to form a polymer.

As used herein, the term “α-olefin” or “alpha-olefin” is used todescribe a monomer having a linear hydrocarbon chain containing from 3to 20 carbon atoms having a double bond at one end of the chain; anequivalent term is “linear α-olefin”.

As used herein, the term “polyethylene” or “ethylene polymer”, refers tomacromolecules produced from ethylene monomers and optionally one ormore additional monomers; regardless of the specific catalyst orspecific process used to make the ethylene polymer. In the polyethyleneart, the one or more additional monomers are called “comonomer(s)” andoften include α-olefins. The term “homopolymer” refers to a polymer thatcontains only one type of monomer. An “ethylene homopolymer” is madeusing only ethylene as a polymerizable monomer. The term “copolymer”refers to a polymer that contains two or more types of monomer. An“ethylene copolymer” is made using ethylene and one or more other typesof polymerizable monomer. Common polyethylenes include high densitypolyethylene (HDPE), medium density polyethylene (MDPE), linear lowdensity polyethylene (LLDPE), very low density polyethylene (VLDPE),ultralow density polyethylene (ULDPE), plastomer and elastomers. Theterm polyethylene also includes polyethylene terpolymers which mayinclude two or more comonomers in addition to ethylene. The termpolyethylene also includes combinations of, or blends of, thepolyethylenes described above.

The term “heterogeneously branched polyethylene” refers to a subset ofpolymers in the ethylene polymer group that are produced using aheterogeneous catalyst system; non-limiting examples of which includeZiegler-Natta or chromium catalysts, both of which are well known in theart.

The term “homogeneously branched polyethylene” refers to a subset ofpolymers in the ethylene polymer group that are produced usingsingle-site catalysts; non-limiting examples of which includemetallocene catalysts, phosphinimine catalysts, and constrained geometrycatalysts all of which are well known in the art.

Typically, homogeneously branched polyethylene has narrow molecularweight distributions, for example gel permeation chromatography (GPC)M_(w)/M_(n) values of less than 2.8, for example less than 2.3, althoughexceptions may arise; M_(w) and M_(n) refer to weight and number averagemolecular weights, respectively. In contrast, the M_(w)/M_(n) ofheterogeneously branched ethylene polymers are typically greater thanthe M_(w)/M_(n) of homogeneous polyethylene. In general, homogeneouslybranched ethylene polymers also have a narrow comonomer distribution,i.e. each macromolecule within the molecular weight distribution has asimilar comonomer content. Frequently, the composition distributionbreadth index “CDBI” is used to quantify how the comonomer isdistributed within an ethylene polymer, as well as to differentiateethylene polymers produced with different catalysts or processes. The“CDBI₅₀” is defined as the percent of ethylene polymer whose compositionis within 50 weight percent (wt. %) of the median comonomer composition;this definition is consistent with that described in WO 93/03093assigned to Exxon Chemical Patents Inc. The CDBI₅₀ of an ethyleneinterpolymer can be calculated from TREF curves (Temperature RisingElution Fractionation); the TREF method is described in Wild, et al., J.Polym. Sci., Part B, Polym. Phys., Vol. 20 (3), pages 441-455.Typically, the CDBI₅₀ of homogeneously branched ethylene polymers aregreater than about 70% or greater than about 75%. In contrast, theCDBI₅₀ of α-olefin containing heterogeneously branched ethylene polymersare generally lower than the CDBI₅₀ of homogeneous ethylene polymers.For example, the CDBI₅₀ of a heterogeneously branched ethylene polymermay be less than about 75%, or less than about 70%.

It is well known to those skilled in the art, that homogeneouslybranched ethylene polymers are frequently further subdivided into“linear homogeneous ethylene polymers” and “substantially linearhomogeneous ethylene polymers”. These two subgroups differ in the amountof long chain branching: for example, linear homogeneous ethylenepolymers have less than about 0.01 long chain branches per 1000 carbonatoms; while substantially linear ethylene polymers have greater thanabout 0.01 to about 3.0 long chain branches per 1000 carbon atoms. Along chain branch is macromolecular in nature, i.e. similar in length tothe macromolecule that the long chain branch is attached to. Hereafter,in this disclosure, the term “homogeneously branched polyethylene” or“homogeneously branched ethylene polymer” refers to both linearhomogeneous ethylene polymers and substantially linear homogeneousethylene polymers.

The term “thermoplastic” refers to a polymer that becomes liquid whenheated, will flow under pressure and solidify when cooled. Thermoplasticpolymers include ethylene polymers as well as other polymers used in theplastic industry; non-limiting examples of other polymers commonly usedin film applications include barrier resins (EVOH), tie resins,polyethylene terephthalate (PET), polyamides and the like.

As used herein the term “monolayer film” refers to a film containing asingle layer of one or more thermoplastics.

As used herein, the terms “hydrocarbyl”, “hydrocarbyl radical” or“hydrocarbyl group” refers to linear or cyclic, aliphatic, olefinic,acetylenic and aryl (aromatic) radicals including hydrogen and carbonthat are deficient by one hydrogen.

As used herein, an “alkyl radical” includes linear, branched and cyclicparaffin radicals that are deficient by one hydrogen radical;non-limiting examples include methyl (—CH₃) and ethyl (—CH₂CH₃)radicals. The term “alkenyl radical” refers to linear, branched andcyclic hydrocarbons containing at least one carbon-carbon double bondthat is deficient by one hydrogen radical.

As used herein, the term “aryl” group includes phenyl, naphthyl, pyridyland other radicals whose molecules have an aromatic ring structure;non-limiting examples include naphthylene, phenanthrene and anthracene.An “arylalkyl” group is an alkyl group having an aryl group pendantthere from; non-limiting examples include benzyl, phenethyl andtolylmethyl; an “alkylaryl” is an aryl group having one or more alkylgroups pendant there from; non-limiting examples include tolyl, xylyl,mesityl and cumyl.

As used herein, the phrase “heteroatom” includes any atom other thancarbon and hydrogen that can be bound to carbon. A“heteroatom-containing group” is a hydrocarbon radical that contains aheteroatom and may contain one or more of the same or differentheteroatoms. In one embodiment, a heteroatom-containing group is ahydrocarbyl group containing from 1 to 3 atoms chosen from boron,aluminum, silicon, germanium, nitrogen, phosphorous, oxygen and sulfur.Non-limiting examples of heteroatom-containing groups include radicalsof imines, amines, oxides, phosphines, ethers, ketones, oxoazolinesheterocyclics, oxazolines, thioethers, and the like. The term“heterocyclic” refers to ring systems having a carbon backbone thatinclude from 1 to 3 atoms chosen from boron, aluminum, silicon,germanium, nitrogen, phosphorous, oxygen and sulfur.

As used herein the term “unsubstituted” means that hydrogen radicals arebounded to the molecular group that follows the term unsubstituted. Theterm “substituted” means that the group following this term possessesone or more moieties that have replaced one or more hydrogen radicals inany position within the group; non-limiting examples of moieties includehalogen radicals (F, Cl, Br), hydroxyl groups, carbonyl groups, carboxylgroups, amine groups, phosphine groups, alkoxy groups, phenyl groups,naphthyl groups, C₁ to C₃₀ alkyl groups, C₂ to C₃₀ alkenyl groups, andcombinations thereof. Non-limiting examples of substituted alkyls andaryls include: acyl radicals, alkylamino radicals, alkoxy radicals,aryloxy radicals, alkylthio radicals, dialkylamino radicals,alkoxycarbonyl radicals, aryloxycarbonyl radicals, carbomoyl radicals,alkyl- and dialkyl-carbamoyl radicals, acyloxy radicals, acylaminoradicals, arylamino radicals and combinations thereof.

In the present disclosure, the polyethylene compositions include atleast the following types of polymers: a first polyethylene which is anethylene copolymer and which has a Mw/Mn of less than about 2.3; asecond polyethylene which is an ethylene copolymer or an ethylenehomopolymer which is different from the first polyethylene and which hasa Mw/Mn of less than about 2.3; and a third polyethylene which is anethylene copolymer or an ethylene homopolymer which has a Mw/Mn ofgreater than about 2.3. Each of these polyethylene components, and thepolyethylene composition of which they are each a part are furtherdescribed below.

The First Polyethylene

In an embodiment of the disclosure, the first polyethylene is made witha single site catalyst, non-limiting examples of which includephosphinimine catalysts, metallocene catalysts, and constrained geometrycatalysts, all of which are well known in the art.

In an embodiment of the disclosure, the first polyethylene is anethylene copolymer. Suitable alpha-olefins which may be copolymerizedwith ethylene to make an ethylene copolymer include 1-propene, 1-butene,1-pentene, 1-hexene and 1-octene.

In an embodiment of the disclosure, the first polyethylene is ahomogeneously branched ethylene copolymer.

In an embodiment of the disclosure, the first polyethylene is anethylene/1-octene copolymer.

In an embodiment of the disclosure, the first polyethylene is made witha phosphinimine catalyst.

In an embodiment of the disclosure, a phosphinimine catalyst isrepresented by formula:

(L^(A))_(a)M(Pl)_(b)(Q)_(n)

wherein (L^(A)) represents is cyclopentadienyl-type ligand; M representsa metal atom chosen from Ti, Zr, and Hf; Pl represents a phosphinimineligand; Q represents an activatable ligand; a is 0 or 1; b is 1 or 2;(a+b)=2; n is 1 or 2, and; the sum of (a+b+n) equals the valance of themetal M.

As used herein, the term “cyclopentadienyl-type” ligand is meant toinclude ligands which contain at least one five-carbon ring which isbonded to the metal via eta-5 (or in some cases eta-3) bonding. Thus,the term “cyclopentadienyl-type” includes, for example, unsubstitutedcyclopentadienyl, singly or multiply substituted cyclopentadienyl,unsubstituted indenyl, singly or multiply substituted indenyl,unsubstituted fluorenyl and singly or multiply substituted fluorenyl.Hydrogenated versions of indenyl and fluorenyl ligands are alsocontemplated for use in the current disclosure, so long as thefive-carbon ring which bonds to the metal via eta-5 (or in some caseseta-3) bonding remains intact. Substituents for a cyclopentadienylligand, an indenyl ligand (or hydrogenated version thereof) and afluorenyl ligand (or hydrogenated version thereof) may be chosen from aC₁₋₃₀ hydrocarbyl radical (which hydrocarbyl radical may beunsubstituted or further substituted by for example a halide and/or ahydrocarbyl group; for example a suitable substituted C₁₋₃₀ hydrocarbylradical is a pentafluorobenzyl group such as —CH₂C₆F₅); a halogen atom;a C₁₋₈ alkoxy radical; a C₆₋₁₀ aryl or aryloxy radical (each of whichmay be further substituted by for example a halide and/or a hydrocarbylgroup); an amido radical which is unsubstituted or substituted by up totwo C₁₋₈ alkyl radicals; a phosphido radical which is unsubstituted orsubstituted by up to two C₁₋₈ alkyl radicals; a silyl radical of theformula —Si(R′)₃ wherein each R′ is independently chosen from hydrogen,a C₁₋₈ alkyl or alkoxy radical, C₆₋₁₀ aryl or aryloxy radicals; and agermanyl radical of the formula —Ge(R′)₃ wherein R′ is as defineddirectly above.

The phosphinimine ligand, PI, is defined by formula:

(R^(p))₃P=N—

wherein the R^(p) groups are independently chosen from: a hydrogen atom;a halogen atom; C₁₋₂₀ hydrocarbyl radicals which are unsubstituted orsubstituted with one or more halogen atom(s); a C₁₋₈ alkoxy radical; aC₆₋₁₀ aryl radical; a C₆₋₁₀ aryloxy radical; an amido radical; a silylradical of formula —Si(R^(s))₃, wherein the R^(s) groups areindependently chosen from, a hydrogen atom, a C₁₋₈ alkyl or alkoxyradical, a C₆₋₁₀ aryl radical, a C₆₋₁₀ aryloxy radical, or a germanylradical of formula —Ge(R^(G))₃, wherein the R^(G) groups are defined asR^(s) is defined in this paragraph.

In an embodiment of the disclosure, the metal, M in the phosphiniminecatalyst is titanium, Ti.

In an embodiment of the disclosure, the single site catalyst used tomake the first polyethylene is cyclopentadienyltri(tertiarybutyl)phosphinimine titanium dichloride, Cp((t-Bu)₃PN)TiCl₂.

In an embodiment of the disclosure, the first polyethylene is made witha metallocene catalyst.

In an embodiment of the disclosure, the first polyethylene is made witha bridged metallocene catalyst.

In an embodiment of the disclosure, the first polyethylene is made witha bridged metallocene catalyst having the formula I:

In Formula (I): M is a group 4 metal chosen from titanium, zirconium orhafnium; G is a group 14 element chosen from carbon, silicon, germanium,tin and lead; R₁ is a hydrogen atom, a C₁₋₂₀ hydrocarbyl radical, aC₁₋₂₀ alkoxy radical or a C₆₋₁₀ aryl oxide radical; R₂ and R₃ areindependently chosen from a hydrogen atom, a C₁₋₂₀ hydrocarbyl radical,a C₁₋₂₀ alkoxy radical or a C₆₋₁₀ aryl oxide radical; R₄ and R₅ areindependently chosen from a hydrogen atom, a C₁₋₂₀ hydrocarbyl radical,a C₁₋₂₀ alkoxy radical or a C₆₋₁₀ aryl oxide radical; and Q isindependently an activatable leaving group ligand.

In the current disclosure, the term “activatable”, means that the ligandQ may be cleaved from the metal center M via a protonolysis reaction orabstracted from the metal center M by suitable acidic or electrophiliccatalyst activator compounds (also known as “co-catalyst” compounds)respectively, examples of which are described below. The activatableligand Q may also be transformed into another ligand which is cleaved orabstracted from the metal center M (e.g. a halide may be converted to analkyl group). Without wishing to be bound by any single theory,protonolysis or abstraction reactions generate an active “cationic”metal center which can polymerize olefins.

In embodiments of the present disclosure, the activatable ligand, Q isindependently chosen from a hydrogen atom; a halogen atom; a C₁₋₂₀hydrocarbyl radical, a C₁₋₂₀ alkoxy radical, and a C₆₋₁₀ aryl or aryloxyradical, where each of the hydrocarbyl, alkoxy, aryl, or aryl oxideradicals may be un-substituted or further substituted by one or morehalogen or other group; a C₁₋₈ alkyl; a C₁₋₈ alkoxy; a C₆₋₁₀ aryl oraryloxy; an amido or a phosphido radical, but where Q is not acyclopentadienyl. Two Q ligands may also be joined to one another andform for example, a substituted or unsubstituted diene ligand (e.g.1,3-butadiene); or a delocalized heteroatom containing group such as anacetate or acetamidinate group. In a convenient embodiment of thedisclosure, each Q is independently chosen from a halide atom, a C₁₋₄alkyl radical and a benzyl radical. Particularly suitable activatableligands Q are monoanionic such as a halide (e.g. chloride) or ahydrocarbyl (e.g. methyl, benzyl).

In an embodiment of the disclosure, the single site catalyst used tomake the first polyethylene isdiphenylmethylene(cyclopentadienyl)(2,7-di-t-butylfuorenyl)hafniumdichloride having the molecular formula: [(2,7-tBu₂Flu)Ph₂C(Cp)HfCl₂].

In an embodiment of the disclosure the single site catalyst used to makethe first polyethylene has isdiphenylmethylene(cyclopentadienyl)(2,7-di-t-butylfuorenyl)hafniumdimethyl having the molecular formula [(2,7-tBu₂Flu)Ph₂C(Cp)HfMe₂].

In addition to the single site catalyst molecule per se, an activesingle site catalyst system may further include one or more of thefollowing: an alkylaluminoxane co-catalyst and an ionic activator. Thesingle site catalyst system may also optionally include a hinderedphenol.

Although the exact structure of alkylaluminoxane is uncertain, subjectmatter experts generally agree that it is an oligomeric species thatcontain repeating units of the general formula:

(R)₂AlO—(Al(R)—O)_(n)—Al(R)₂

where the R groups may be the same or different linear, branched orcyclic hydrocarbyl radicals containing 1 to 20 carbon atoms and n isfrom 0 to about 50. A non-limiting example of an alkylaluminoxane ismethylaluminoxane (or MAO) wherein each R group is a methyl radical.

In an embodiment of the disclosure, R of the alkylaluminoxane, is amethyl radical and m is from 10 to 40.

In an embodiment of the disclosure, the co-catalyst is modifiedmethylaluminoxane (MMAO).

It is well known in the art, that the alkylaluminoxane can serve dualroles as both an alkylator and an activator. Hence, an alkylaluminoxaneco-catalyst is often used in combination with activatable ligands suchas halogens.

In general, ionic activators are comprised of a cation and a bulkyanion; wherein the latter is substantially non-coordinating.Non-limiting examples of ionic activators are boron ionic activatorsthat are four coordinate with four ligands bonded to the boron atom.Non-limiting examples of boron ionic activators include the followingformulas shown below;

[R₅]⁺[B(R⁷)₄]⁻

where B represents a boron atom, R⁵ is an aromatic hydrocarbyl (e.g.triphenyl methyl cation) and each R⁷ is independently chosen from phenylradicals which are unsubstituted or substituted with from 3 to 5substituents chosen from fluorine atoms, C₁₋₄ alkyl or alkoxy radicalswhich are unsubstituted or substituted by fluorine atoms; and a silylradical of formula —Si(R⁹)₃, where each R⁹ is independently chosen fromhydrogen atoms and C₁₋₄ alkyl radicals, and

[(R₈)_(t)ZH]⁺[B(R⁷)₄]⁻

where B is a boron atom, H is a hydrogen atom, Z is a nitrogen orphosphorus atom, t is 2 or 3 and R⁸ is chosen from C₁₋₈ alkyl radicals,and phenyl radicals which are unsubstituted or substituted by up tothree C₁₋₄ alkyl radicals, or wherein one R⁸ taken together with thenitrogen atom may form an anilinium radical and R⁷ is as defined above.

In both formula a non-limiting example of R⁷ is a pentafluorophenylradical. In general, boron ionic activators may be described as salts oftetra(perfluorophenyl) boron; non-limiting examples include anilinium,carbonium, oxonium, phosphonium and sulfonium salts oftetra(perfluorophenyl)boron with anilinium and trityl (ortriphenylmethylium). Additional non-limiting examples of ionicactivators include: triethylammonium tetra(phenyl)boron,tripropylammonium tetra(phenyl)boron, tri(n-butyl)ammoniumtetra(phenyl)boron, trimethylammonium tetra(p-tolyl)boron,trimethylammonium tetra(o-tolyl)boron, tributylammoniumtetra(pentafluorophenyl)boron, tripropylammoniumtetra(o,p-dimethylphenyl)boron, tributylammoniumtetra(m,m-dimethylphenyl)boron, tributylammoniumtetra(p-trifluoromethylphenyl)boron, tributylammoniumtetra(pentafluorophenyl)boron, tri(n-butyl)ammonium tetra(o-tolyl)boron,N,N-dimethylanilinium tetra(phenyl)boron, N,N-diethylaniliniumtetra(phenyl)boron, N,N-diethylanilinium tetra(phenyl)n-butylboron,N,N-2,4,6-pentamethylanilinium tetra(phenyl)boron,di-(isopropyl)ammonium tetra(pentafluorophenyl) boron,dicyclohexylammonium tetra(phenyl)boron, triphenylphosphoniumtetra(phenyl)boron, tri(methylphenyl)phosphonium tetra(phenyl)boron,tri(dimethylphenyl)phosphonium tetra(phenyl)boron, tropilliumtetrakispentafluorophenyl borate, triphenylmethyliumtetrakispentafluorophenyl borate,benzene(diazonium)tetrakispentafluorophenyl borate, tropilliumtetrakis(2,3,5,6-tetrafluorophenyl)borate, triphenylmethyliumtetrakis(2,3,5,6-tetrafluorophenyl)borate, benzene(diazonium)tetrakis(3,4,5-trifluorophenyl)borate, tropilliumtetrakis(3,4,5-trifluorophenyl)borate, benzene(diazonium)tetrakis(3,4,5-trifluorophenyl)borate, tropilliumtetrakis(1,2,2-trifluoroethenyl)borate, triphenylmethyliumtetrakis(1,2,2-trifluoroethenyl)borate, benzene(diazonium)tetrakis(1,2,2-trifluoroethenyl)borate, tropilliumtetrakis(2,3,4,5-tetrafluorophenyl)borate, triphenylmethyliumtetrakis(2,3,4,5-tetrafluorophenyl)borate, and benzene(diazonium)tetrakis(2,3,4,5 tetrafluorophenyl)borate. Readily available commercialionic activators include N,N-dimethylanilinium tetrakispentafluorophenylborate, and triphenylmethylium tetrakispentafluorophenyl borate.

Non-limiting example of hindered phenols include butylated phenolicantioxidants, butylated hydroxytoluene, 2,6-di-tertiarybutyl-4-ethylphenol, 4,4′-methylenebis (2,6-di-tertiary-butylphenol),1,3,5-trimethyl-2,4,6-tris (3,5-di-tert-butyl-4-hydroxybenzyl) benzeneand octadecyl-3-(3′,5′-di-tert-butyl-4′-hydroxyphenyl) propionate.

To produce an active single site catalyst system the quantity and moleratios of the three or four components: the single site catalyst, thealkylaluminoxane, the ionic activator, and the optional hindered phenolare optimized.

In an embodiment of the disclosure, the single site catalyst used tomake the first polyethylene produces no long chain branches, and thefirst polyethylene will contain no measurable amounts of long chainbranches.

In an embodiment of the disclosure, the single site catalyst used tomake the first polyethylene produces long chain branches, and the firstpolyethylene will contain long chain branches, hereinafter “LCB”. LCB isa well-known structural phenomenon in polyethylenes and well known tothose of ordinary skill in the art. Traditionally, there are threemethods for LCB analysis, namely, nuclear magnetic resonancespectroscopy (NMR), for example see J. C. Randall, J Macromol. Sci.,Rev. Macromol. Chem. Phys. 1989, 29, 201; triple detection SEC equippedwith a DRI, a viscometer and a low-angle laser light scatteringdetector, for example see W. W. Yau and D. R. Hill, Int. J. Polym. Anal.Charact. 1996; 2:151; and rheology, for example see W. W. Graessley,Acc. Chem. Res. 1977, 10, 332-339. In this disclosure, a long chainbranch is macromolecular in nature, i.e. long enough to be seen in anNMR spectra, triple detector SEC experiments or rheological experiments.

In embodiments of the disclosure, the upper limit on the molecularweight distribution, M_(w)/M_(n) of the first polyethylene may be about2.8, or about 2.5, or about 2.4, or about 2.3, or about 2.2. Inembodiments of the disclosure, the lower limit on the molecular weightdistribution, M_(w)/M_(n) of the first polyethylene may be about 1.4, orabout 1.6, or about 1.7, or about 1.8, or about 1.9.

In embodiments of the disclosure, the first polyethylene has a molecularweight distribution, M_(w)/M_(n) of <2.3, or <2.1, or <2.0 or about 2.0.In embodiments of the disclosure, the first polyethylene has a molecularweight distribution, M_(w)/M_(n) of from about 1.7 to about 2.2.

In an embodiment of the disclosure, the first polyethylene has from 1 to200 short chain branches per thousand carbon atoms (SCB_(PE-1)). Infurther embodiments, the first polyethylene has from 3 to 150 shortchain branches per thousand carbon atoms (SCB_(PE-1)), or from 5 to 100short chain branches per thousand carbon atoms (SCB_(PE-1)), or from 10to 100 short chain branches per thousand carbon atoms (SCB_(PE-1)), orfrom 5 to 75 short chain branches per thousand carbon atoms(SCB_(PE-1)), or from 10 to 75 short chain branches per thousand carbonatoms (SCB_(PE-1)), or from 15 to 75 short chain branches per thousandcarbon atoms (SCB_(PE-1)), or from 20 to 75 short chain branches perthousand carbon atoms (SCB_(PE-1)). In still further embodiments, thefirst polyethylene has from 20 to 100 short chain branches per thousandcarbon atoms (SCB_(PE-1)), or from 25 to 100 short chain branches perthousand carbon atoms (SCB_(PE-1)), or from 30 to 100 short chainbranches per thousand carbon atoms (SCB_(PE-1)), or from 35 to 100 shortchain branches per thousand carbon atoms (SCB_(PE-1)), or from 35 to 75short chain branches per thousand carbon atoms (SCB_(PE-1)), or from 30to 75 short chain branches per thousand carbon atoms (SCB_(PE-1)), orfrom 30 to 60 short chain branches per thousand carbon atoms(SCB_(PE-1)), or from 30 to 50 short chain branches per thousand carbonatoms (SCB_(PE-1)), or from 35 to 60 short chain branches per thousandcarbon atoms (SCB_(PE-1)), or from 35 to 55 short chain branches perthousand carbon atoms (SCB_(PE-1)).

The short chain branching (i.e. the short chain branching per thousandcarbons, SCB_(PE-1)) is the branching due to the presence of analpha-olefin comonomer in the polyethylene and will for example have twocarbon atoms for a 1-butene comonomer, or four carbon atoms for a1-hexene comonomer, or six carbon atoms for a 1-octene comonomer, etc.

In an embodiment of the disclosure, the number of short chain branchesper thousand carbon atoms in the first polyethylene (SCB_(PE-1)), isgreater than the number of short chain branches per thousand carbonatoms in the second polyethylene (SCB_(PE-2)).

In an embodiment of the disclosure, the number of short chain branchesper thousand carbon atoms in the first polyethylene (SCB_(PE-1)), isgreater than the number of short chain branches per thousand carbonatoms in the third polyethylene (SCB_(PE-3)).

In an embodiment of the disclosure, the number of short chain branchesper thousand carbon atoms in the first polyethylene (SCB_(PE-1)), isgreater than the number of short chain branches per thousand carbonatoms in each of the second polyethylene (SCB_(PE-2)) and the thirdpolyethylene (SCB_(PE-3)).

In embodiments of the disclosure, the upper limit on the density, d1 ofthe first polyethylene may be about 0.975 g/cm³; in some cases about0.965 g/cm³ and; in other cases about 0.955 g/cm³. In embodiments of thedisclosure, the lower limit on the density, d1 of the first polyethylenemay be about 0.855 g/cm³, in some cases about 0.865 g/cm³, and; in othercases about 0.875 g/cm³.

In embodiments of the disclosure the density, d1 of the firstpolyethylene may be from about 0.855 to about 0.965 g/cm³, or from 0.865g/cm³ to about 0.965 g/cm³, or from about 0.870 g/cm³ to about 0.960g/cm³, or from about 0.865 g/cm³ to 0.950 g/cm³, or from about 0.865g/cm³ to about 0.940 g/cm³, or from about 0.865 g/cm³ to about 0.936g/cm³, or from about 0.860 g/cm³ to about 0.932 g/cm³, or from about0.865 g/cm³ to about 0.926 g/cm³, or from about 0.865 g/cm³ to about0.921 g/cm³, or from about 0.865 g/cm³ to about 0.918 g/cm³, or fromabout 0.865 g/cm³ to about 0.916 g/cm³, or from about 0.870 g/cm³ toabout 0.916 g/cm³, or from about 0.865 g/cm³ to about 0.912 g/cm³, orfrom about 0.865 g/cm³ to about 0.910 g/cm³, or from about 0.865 g/cm³to about 0.905 g/cm³, or from about 0.865 g/cm³ to about 0.900 g/cm³, orfrom about 0.855 g/cm³ to about 0.900 g/cm³, or from about 0.855 g/cm³to about 0.905 g/cm³, or from about 0.855 g/cm³ to about 0.910 g/cm³, orfrom about 0.855 g/cm³ to about 0.916 g/cm³.

In embodiments of the disclosure, the upper limit on the CDBI₅₀ of thefirst polyethylene may be about 98 weight %, in other cases about 95 wt% and in still other cases about 90 wt. %. In embodiments of thedisclosure, the lower limit on the CDBI₅₀ of the first polyethylene maybe about 70 weight %, in other cases about 75 wt. % and in still othercases about 80 wt. %.

In embodiments of the disclosure the melt index of the firstpolyethylene I₂ ¹ may be from about 0.01 dg/min to about 1000 dg/min, orfrom about 0.01 dg/min to about 500 dg/min, or from about 0.01 dg/min toabout 100 dg/min, or from about 0.01 dg/min to about 50 dg/min, or fromabout 0.01 dg/min to about 25 dg/min, or from about 0.01 dg/min to about10 dg/min, or from about 0.01 dg/min to about 5 dg/min, or from about0.01 dg/min to about 3 dg/min, or from about 0.01 dg/min to about 1dg/min, or less than about 5 dg/min, or less than about 3 dg/min, orless than about 1.0 dg/min, or less than about 0.75 dg/min, or less thanabout 0.50 dg/min.

In an embodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) of from about 50,000 to about 300,000,or from about 50,000 to about 250,000, or from about 60,000 to about250,000, or from about 70,000 to about 250,000 or from about 60,000 toabout 220,000, or from about 70,000 to about 200,000, or from about75,000 to about 200,000, or from about 75,000 to about 175,000; or fromabout 70,000 to about 175,000, or from about 70,000 to about 150,000.

In an embodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) which is greater than the weight averagemolecular weight, M_(w) of the second polyethylene.

In an embodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) which is greater than the weight averagemolecular weight, M_(w) of the third polyethylene.

In an embodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) which is within 30 percent of the weightaverage molecular weight, M_(w) of the third polyethylene. For clarity,this means that: the absolute difference between the weight averagemolecular weight, M_(w) of the first polyethylene and the weight averagemolecular weight, M_(w) of the third polyethylene divided by the weightaverage molecular weight, M_(w) of the third polyethylene and convertedto a percentage (i.e. [Mw1−Mw3/Mw3]×100%) is within 25 percent.

In an embodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) which is within 25 percent of the weightaverage molecular weight, M_(w) of the third polyethylene. In anembodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) which is within 20 percent of the weightaverage molecular weight, M_(w) of the third polyethylene. In anembodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) which is within 15 percent of the weightaverage molecular weight, M_(w) of the third polyethylene. In anembodiment of the disclosure, the first polyethylene has a weightaverage molecular weight, M_(w) which is within 10 percent of the weightaverage molecular weight, M_(w) of the third polyethylene.

In embodiments of the disclosure, the upper limit on the weight percent(wt. %) of the first polyethylene in the polyethylene composition (i.e.the weight percent of the first polyethylene based on the total weightof the first, the second and the third polyethylene) may be about 80 wt.%, or about 75 wt. %, or about 70 wt. %, or about 65 wt. %, or about 60wt. %, or about 55 wt. % or about 50 wt. %, or about 45%, or about 40%,or about 35%. In embodiments of the disclosure, the lower limit on thewt. % of the first polyethylene in the polyethylene composition may beabout 1 wt. %, or about 5 wt. %, or about 10 wt. %, or about 15 wt. %,or about 20 wt. %, or about 25 wt. % or in other cases about 30 wt. %.

The Second Polyethylene

In an embodiment of the disclosure, the second polyethylene is made witha single site catalyst, non-limiting examples of which includephosphinimine catalysts, metallocene catalysts, and constrained geometrycatalysts, all of which are well known in the art.

In an embodiment of the disclosure, the second polyethylene is anethylene homopolymer.

In an embodiment of the disclosure, the second polyethylene is anethylene copolymer. Suitable alpha-olefins which may be copolymerizedwith ethylene to make an ethylene copolymer include 1-propene, 1-butene,1-pentene, 1-hexene and 1-octene.

In an embodiment of the disclosure, the second polyethylene is ahomogeneously branched ethylene copolymer.

In an embodiment of the disclosure, the second polyethylene is anethylene/1-octene copolymer.

In an embodiment of the disclosure, the second polyethylene is made witha phosphinimine catalyst.

In an embodiment of the disclosure, a phosphinimine catalyst isrepresented by formula:

(L^(A))_(a)M(Pl)_(b)(Q)_(n)

wherein (L^(A)) represents is cyclopentadienyl-type ligand; M representsa metal atom chosen from Ti, Zr, and Hf; Pl represents a phosphinimineligand; Q represents an activatable ligand; a is 0 or 1; b is 1 or 2;(a+b)=2; n is 1 or 2, and; the sum of (a+b+n) equals the valance of themetal M.

As used herein, the term “cyclopentadienyl-type” ligand is meant toinclude ligands which contain at least one five-carbon ring which isbonded to the metal via eta-5 (or in some cases eta-3) bonding. Thus,the term “cyclopentadienyl-type” includes, for example, unsubstitutedcyclopentadienyl, singly or multiply substituted cyclopentadienyl,unsubstituted indenyl, singly or multiply substituted indenyl,unsubstituted fluorenyl and singly or multiply substituted fluorenyl.Hydrogenated versions of indenyl and fluorenyl ligands are alsocontemplated for use in the current disclosure, so long as thefive-carbon ring which bonds to the metal via eta-5 (or in some caseseta-3) bonding remains intact. Substituents for a cyclopentadienylligand, an indenyl ligand (or hydrogenated version thereof) and afluorenyl ligand (or hydrogenated version thereof) may be chosen from aC₁₋₃₀ hydrocarbyl radical (which hydrocarbyl radical may beunsubstituted or further substituted by for example a halide and/or ahydrocarbyl group; for example a suitable substituted C₁-30 hydrocarbylradical is a pentafluorobenzyl group such as —CH₂C₆F₅); a halogen atom;a C₁₋₈ alkoxy radical; a C₆₋₁₀ aryl or aryloxy radical (each of whichmay be further substituted by for example a halide and/or a hydrocarbylgroup); an amido radical which is unsubstituted or substituted by up totwo C₁₋₈ alkyl radicals; a phosphido radical which is unsubstituted orsubstituted by up to two C₁₋₈ alkyl radicals; a silyl radical of theformula —Si(R′)₃ wherein each R′ is independently chosen from hydrogen,a C₁₋₈ alkyl or alkoxy radical, C₆₋₁₀ aryl or aryloxy radicals; and agermanyl radical of the formula —Ge(R′)₃ wherein R′ is as defineddirectly above.

The phosphinimine ligand, PI, is defined by formula:

(R^(p))₃P=N—

wherein the R^(p) groups are independently chosen from: a hydrogen atom;a halogen atom; C₁₋₂₀ hydrocarbyl radicals which are unsubstituted orsubstituted with one or more halogen atom(s); a C₁₋₈ alkoxy radical; aC₆₋₁₀ aryl radical; a C₆₋₁₀ aryloxy radical; an amido radical; a silylradical of formula —Si(R^(s))₃, wherein the R^(s) groups areindependently chosen from, a hydrogen atom, a C₁₋₈ alkyl or alkoxyradical, a C₆₋₁₀ aryl radical, a C₆₋₁₀ aryloxy radical, or a germanylradical of formula —Ge(R^(G))₃, wherein the R^(G) groups are defined asR^(s) is defined in this paragraph.

In an embodiment of the disclosure, the metal, M in the phosphiniminecatalyst is titanium, Ti.

In an embodiment of the disclosure, the single site catalyst used tomake the second polyethylene is cyclopentadienyltri(tertiarybutyl)phosphinimine titanium dichloride, Cp((t-Bu)₃PN)TiCl₂.

In an embodiment of the disclosure, the second polyethylene is made witha metallocene catalyst.

In an embodiment of the disclosure, the second polyethylene is made witha bridged metallocene catalyst.

In an embodiment of the disclosure, the second polyethylene is made witha bridged metallocene catalyst having the formula I:

In Formula (I): M is a group 4 metal chosen from titanium, zirconium orhafnium; G is a group 14 element chosen from carbon, silicon, germanium,tin or lead; R₁ is a hydrogen atom, a C₁₋₂₀ hydrocarbyl radical, a C₁₋₂₀alkoxy radical or a C₆₋₁₀ aryl oxide radical; R₂ and R₃ areindependently chosen from a hydrogen atom, a C₁₋₂₀ hydrocarbyl radical,a C₁₋₂₀ alkoxy radical or a C₆₋₁₀ aryl oxide radical; R₄ and R₅ areindependently chosen from a hydrogen atom, a C₁₋₂₀ hydrocarbyl radical,a C₁₋₂₀ alkoxy radical or a C₆₋₁₀ aryl oxide radical; and Q isindependently an activatable leaving group ligand.

In the current disclosure, the term “activatable”, means that the ligandQ may be cleaved from the metal center M via a protonolysis reaction orabstracted from the metal center M by suitable acidic or electrophiliccatalyst activator compounds (also known as “co-catalyst” compounds)respectively, examples of which are described below. The activatableligand Q may also be transformed into another ligand which is cleaved orabstracted from the metal center M (e.g. a halide may be converted to analkyl group). Without wishing to be bound by any single theory,protonolysis or abstraction reactions generate an active “cationic”metal center which can polymerize olefins.

In embodiments of the present disclosure, the activatable ligand, Q isindependently chosen from a hydrogen atom; a halogen atom; a C₁₋₂₀hydrocarbyl radical, a C₁₋₂₀ alkoxy radical, and a C₆₋₁₀ aryl or aryloxyradical, where each of the hydrocarbyl, alkoxy, aryl, or aryl oxideradicals may be un-substituted or further substituted by one or morehalogen or other group; a C₁₋₈ alkyl; a C₁₋₈ alkoxy; a C₆₋₁₀ aryl oraryloxy; an amido or a phosphido radical, but where Q is not acyclopentadienyl. Two Q ligands may also be joined to one another andform for example, a substituted or unsubstituted diene ligand (e.g.1,3-butadiene); or a delocalized heteroatom containing group such as anacetate or acetamidinate group. In a convenient embodiment of thedisclosure, each Q is independently chosen from a halide atom, a C₁₋₄alkyl radical and a benzyl radical. Particularly suitable activatableligands Q are monoanionic such as a halide (e.g. chloride) or ahydrocarbyl (e.g. methyl, benzyl).

In an embodiment of the disclosure, the single site catalyst used tomake the second polyethylene isdiphenylmethylene(cyclopentadienyl)(2,7-di-t-butylfuorenyl)hafniumdichloride having the molecular formula: [(2,7-tBu₂Flu)Ph₂C(Cp)HfCl₂].

In an embodiment of the disclosure the single site catalyst used to makethe second polyethylene has isdiphenylmethylene(cyclopentadienyl)(2,7-di-t-butylfuorenyl)hafniumdimethyl having the molecular formula [(2,7-tBu₂Flu)Ph₂C(Cp)HfMe₂].

In addition to the single site catalyst molecule per se, an activesingle site catalyst system may further include one or more of thefollowing: an alkylaluminoxane co-catalyst and an ionic activator. Thesingle site catalyst system may also optionally include a hinderedphenol.

Although the exact structure of alkylaluminoxane is uncertain, subjectmatter experts generally agree that it is an oligomeric species thatcontain repeating units of the general formula:

(R)₂AlO—(Al(R)—O)_(n)—Al(R)₂

where the R groups may be the same or different linear, branched orcyclic hydrocarbyl radicals containing 1 to 20 carbon atoms and n isfrom 0 to about 50. A non-limiting example of an alkylaluminoxane ismethylaluminoxane (or MAO) wherein each R group is a methyl radical.

In an embodiment of the disclosure, R of the alkylaluminoxane, is amethyl radical and m is from 10 to 40.

In an embodiment of the disclosure, the co-catalyst is modifiedmethylaluminoxane (MMAO).

It is well known in the art, that the alkylaluminoxane can serve dualroles as both an alkylator and an activator. Hence, an alkylaluminoxaneco-catalyst is often used in combination with activatable ligands suchas halogens.

In general, ionic activators are comprised of a cation and a bulkyanion; wherein the latter is substantially non-coordinating.Non-limiting examples of ionic activators are boron ionic activatorsthat are four coordinate with four ligands bonded to the boron atom.Non-limiting examples of boron ionic activators include the followingformulas shown below;

[R₅]⁺[B(R⁷)₄]⁻

where B represents a boron atom, R⁵ is an aromatic hydrocarbyl (e.g.triphenyl methyl cation) and each R⁷ is independently chosen from phenylradicals which are unsubstituted or substituted with from 3 to 5substituents chosen from fluorine atoms, C₁₋₄ alkyl or alkoxy radicalswhich are unsubstituted or substituted by fluorine atoms; and a silylradical of formula —Si(R⁹)₃, where each R⁹ is independently chosen fromhydrogen atoms and C₁₋₄ alkyl radicals, and

[(R⁸)_(t)ZH]⁺[B(R⁷)₄]⁻

where B is a boron atom, H is a hydrogen atom, Z is a nitrogen orphosphorus atom, t is 2 or 3 and R⁸ is chosen from C₁₋₈ alkyl radicals,phenyl radicals which are unsubstituted or substituted by up to threeC₁₋₄ alkyl radicals, or wherein one R⁸ taken together with the nitrogenatom may form an anilinium radical and R⁷ is as defined above.

In both formula a non-limiting example of R⁷ is a pentafluorophenylradical. In general, boron ionic activators may be described as salts oftetra(perfluorophenyl) boron; non-limiting examples include anilinium,carbonium, oxonium, phosphonium and sulfonium salts oftetra(perfluorophenyl)boron with anilinium and trityl (ortriphenylmethylium). Additional non-limiting examples of ionicactivators include: triethylammonium tetra(phenyl)boron,tripropylammonium tetra(phenyl)boron, tri(n-butyl)ammoniumtetra(phenyl)boron, trimethylammonium tetra(p-tolyl)boron,trimethylammonium tetra(o-tolyl)boron, tributylammoniumtetra(pentafluorophenyl)boron, tripropylammoniumtetra(o,p-dimethylphenyl)boron, tributylammoniumtetra(m,m-dimethylphenyl)boron, tributylammoniumtetra(p-trifluoromethylphenyl)boron, tributylammoniumtetra(pentafluorophenyl)boron, tri(n-butyl)ammonium tetra(o-tolyl)boron,N,N-dimethylanilinium tetra(phenyl)boron, N,N-diethylaniliniumtetra(phenyl)boron, N,N-diethylanilinium tetra(phenyl)n-butylboron,N,N-2,4,6-pentamethylanilinium tetra(phenyl)boron,di-(isopropyl)ammonium tetra(pentafluorophenyl)boron,dicyclohexylammonium tetra(phenyl)boron, triphenylphosphoniumtetra(phenyl)boron, tri(methylphenyl)phosphonium tetra(phenyl)boron,tri(dimethylphenyl)phosphonium tetra(phenyl)boron, tropilliumtetrakispentafluorophenyl borate, triphenylmethyliumtetrakispentafluorophenyl borate,benzene(diazonium)tetrakispentafluorophenyl borate, tropilliumtetrakis(2,3,5,6-tetrafluorophenyl)borate, triphenylmethyliumtetrakis(2,3,5,6-tetrafluorophenyl)borate, benzene(diazonium)tetrakis(3,4,5-trifluorophenyl)borate, tropilliumtetrakis(3,4,5-trifluorophenyl)borate, benzene(diazonium)tetrakis(3,4,5-trifluorophenyl)borate, tropilliumtetrakis(1,2,2-trifluoroethenyl)borate, triphenylmethyliumtetrakis(1,2,2-trifluoroethenyl)borate, benzene(diazonium)tetrakis(1,2,2-trifluoroethenyl)borate, tropilliumtetrakis(2,3,4,5-tetrafluorophenyl)borate, triphenylmethyliumtetrakis(2,3,4,5-tetrafluorophenyl)borate, and benzene(diazonium)tetrakis(2,3,4,5 tetrafluorophenyl)borate. Readily available commercialionic activators include N,N-dimethylanilinium tetrakispentafluorophenylborate, and triphenylmethylium tetrakispentafluorophenyl borate.

Non-limiting example of hindered phenols include butylated phenolicantioxidants, butylated hydroxytoluene, 2,6-di-tertiarybutyl-4-ethylphenol, 4,4′-methylenebis (2,6-di-tertiary-butylphenol),1,3,5-trimethyl-2,4,6-tris (3,5-di-tert-butyl-4-hydroxybenzyl) benzeneand octadecyl-3-(3′,5′-di-tert-butyl-4′-hydroxyphenyl) propionate.

To produce an active single site catalyst system the quantity and moleratios of the three or four components: the single site catalyst, thealkylaluminoxane, the ionic activator, and the optional hindered phenolare optimized.

In an embodiment of the disclosure, the single site catalyst used tomake the second polyethylene produces no long chain branches, and thesecond polyethylene will contain no measurable amounts of long chainbranches.

In an embodiment of the disclosure, the single site catalyst used tomake the second polyethylene produces long chain branches, and thesecond polyethylene will contain long chain branches, hereinafter “LCB”.LCB is a well-known structural phenomenon in polyethylenes and wellknown to those of ordinary skill in the art. Traditionally, there arethree methods for LCB analysis, namely, nuclear magnetic resonancespectroscopy (NMR), for example see J. C. Randall, J Macromol. Sci.,Rev. Macromol. Chem. Phys. 1989, 29, 201; triple detection SEC equippedwith a DRI, a viscometer and a low-angle laser light scatteringdetector, for example see W. W. Yau and D. R. Hill, Int. J. Polym. Anal.Charact. 1996; 2:151; and rheology, for example see W. W. Graessley,Acc. Chem. Res. 1977, 10, 332-339. In this disclosure, a long chainbranch is macromolecular in nature, i.e. long enough to be seen in anNMR spectra, triple detector SEC experiments or rheological experiments.

In embodiments of the disclosure, the upper limit on the molecularweight distribution, M_(w)/M_(n) of the second polyethylene may be about2.8, or about 2.5, or about 2.4, or about 2.3, or about 2.2. Inembodiments of the disclosure, the lower limit on the molecular weightdistribution, M_(w)/M_(n) of the second polyethylene may be about 1.4,or about 1.6, or about 1.7, or about 1.8, or about 1.9.

In embodiments of the disclosure, the second polyethylene has amolecular weight distribution, M_(w)/M_(n) of <2.3, or <2.1, or <2.0 orabout 2.0. In embodiments of the disclosure, the second polyethylene hasa molecular weight distribution, M_(w)/M_(n) of from about 1.7 to about2.2.

In an embodiment of the disclosure, the second polyethylene has from 0to 100 short chain branches per thousand carbon atoms (SCB_(PE-2)). Infurther embodiments, the second polyethylene has from 0 to 30 shortchain branches per thousand carbon atoms (SCB_(PE-2)), or from 0 to 20short chain branches per thousand carbon atoms (SCB_(PE-2)), or from 0to 15 short chain branches per thousand carbon atoms (SCB_(PE-2)), orfrom 0 to 10 short chain branches per thousand carbon atoms(SCB_(PE-2)), or from 0 to 5 short chain branches per thousand carbonatoms (SCB_(PE-2)), or fewer than 5 short chain branches per thousandcarbon atoms (SCB_(PE-2)), or fewer than 3 short chain branches perthousand carbon atoms (SCB_(PE-2)), or fewer than 1 short chain branchesper thousand carbon atoms (SCB_(PE2)), or about zero short chainbranches per thousand carbon atoms (SCB_(PE-2)).

The short chain branching (i.e. the short chain branching per thousandcarbons, SCB_(PE-1)) is the branching due to the presence of analpha-olefin comonomer in the polyethylene and will for example have twocarbon atoms for a 1-butene comonomer, or four carbon atoms for a1-hexene comonomer, or six carbon atoms for a 1-octene comonomer, etc.

In embodiments of the disclosure, the upper limit on the density, d2 ofthe second polyethylene may be about 0.985 g/cm³; in some cases, about0.975 g/cm³ and; in other cases, about 0.965 g/cm³. In embodiments ofthe disclosure, the lower limit on the density, d2 of the secondpolyethylene may be about 0.921 g/cm³, in some cases about 0.932 g/cm³,and; in other cases about 0.949 g/cm³.

In embodiments of the disclosure the density, d2 of the secondpolyethylene may be from about 0.921 g/cm³ to about 0.980 g/cm³, or fromabout 0.921 g/cm³ to about 0.975 g/cm³, or from about 0.926 g/cm³ toabout 0.975 g/cm³, or from about 0.930 g/cm³ to about 0.975 g/cm³, orfrom about 0.936 g/cm³ to about 0.975 g/cm³, or from about 0.940 g/cm³to about 0.975 g/cm³, or from about 0.940 g/cm³ to about 0.980 g/cm³, orfrom about 0.945 g/cm³ to about 0.975 g/cm³, or from about 0.950 g/cm³to about 0.975 g/cm³, or from about 0.951 g/cm³ to about 0.975 g/cm³, orfrom about 0.953 g/cm³ to about 0.975 g/cm³, or from about 0.953 g/cm³to about 0.985 g/cm³.

In embodiments of the disclosure the melt index of the secondpolyethylene I₂ ² may be from about 0.01 dg/min to about 1000 dg/min, orfrom about 0.01 dg/min to about 500 dg/min, or from about 0.01 dg/min toabout 100 dg/min, or from about 0.01 dg/min to about 50 dg/min, or fromabout 0.1 dg/min to about 100 dg/min, or from about 0.1 dg/min to about75 dg/min, or from about 0.1 dg/min to about 50 dg/min, or from about 1dg/min to about 50 dg/min, or from about 1 dg/min to about 40 dg/min, orfrom about 1 dg/min to about 30 dg/min, or from about 1 dg/min to about25 dg/min, or from about 3 dg/min to about 25 dg/min, or from about 5dg/min to about 20 dg/min.

In an embodiment of the disclosure, the second polyethylene has a weightaverage molecular weight, M_(w) of from about 10,000 to about 150,000,or from about 10,000 to about 125,000, or from about 15,000 to about100,000, or from about 15,000 to about 90,000, or from about 15,000 toabout 80,000 or from about 20,000 to about 75,000, or from about 25,000to about 90,000, or from about 25,000 to about 80,000, or from about25,000 to about 75,000.

In an embodiment of the disclosure, the weight average molecular weightof the second polyethylene is less than the weight average molecularweight of the first polyethylene.

In an embodiment of the disclosure, the weight average molecular weightof the second polyethylene is less than the weight average molecularweight of the third polyethylene.

In an embodiment of the disclosure, the weight average molecular weightof the second polyethylene is less than the weight average molecularweight of both the first polyethylene and the third polyethylene.

In embodiments of the disclosure, the upper limit on the weight percent(wt. %) of the second polyethylene in the polyethylene composition (i.e.the weight percent of the second polyethylene based on the total weightof the first, the second and the third polyethylene) may be about 80 wt.%, or about 75 wt. %, or about 70 wt. %, or about 65 wt. %, or about 60wt. %, or about 55 wt. %, or about 50 wt. %, or about 45 wt. %, or about40 wt. %. In embodiments of the disclosure, the lower limit on the wt. %of the second polyethylene in the polyethylene composition may be about5 wt. %, or about 10 wt. %, or about 15 wt. %, or about 20 wt. %.

The Third Polyethylene

In an embodiment of the disclosure, the third polyethylene is made witha multi-site catalyst system, non-limiting examples of which includeZiegler-Natta catalysts and chromium catalysts, both of which are wellknown in the art.

In an embodiment of the disclosure, the third polyethylene is made witha Ziegler-Natta catalyst.

Ziegler-Natta catalyst systems are well known to those skilled in theart. A Ziegler-Natta catalyst may be an in-line Ziegler-Natta catalystsystem or a batch Ziegler-Natta catalyst system. The term “in-lineZiegler-Natta catalyst system” refers to the continuous synthesis of asmall quantity of an active Ziegler-Natta catalyst system andimmediately injecting this catalyst into at least one continuouslyoperating reactor, wherein the catalyst polymerizes ethylene and one ormore optional α-olefins to form an ethylene polymer. The terms “batchZiegler-Natta catalyst system” or “batch Ziegler-Natta procatalyst”refer to the synthesis of a much larger quantity of catalyst orprocatalyst in one or more mixing vessels that are external to, orisolated from, the continuously operating solution polymerizationprocess. Once prepared, the batch Ziegler-Natta catalyst system, orbatch Ziegler-Natta procatalyst, is transferred to a catalyst storagetank. The term “procatalyst” refers to an inactive catalyst system(inactive with respect to ethylene polymerization); the procatalyst isconverted into an active catalyst by adding an alkyl aluminumco-catalyst. As needed, the procatalyst is pumped from the storage tankto at least one continuously operating reactor, wherein an activecatalyst polymerizes ethylene and one or more optional α-olefins to forma polyethylene. The procatalyst may be converted into an active catalystin the reactor or external to the reactor, or on route to the reactor.

A wide variety of compounds can be used to synthesize an activeZiegler-Natta catalyst system. The following describes various compoundsthat may be combined to produce an active Ziegler-Natta catalyst system.Those skilled in the art will understand that the embodiments in thisdisclosure are not limited to the specific compounds disclosed.

An active Ziegler-Natta catalyst system may be formed from: a magnesiumcompound, a chloride compound, a metal compound, an alkyl aluminumco-catalyst and an aluminum alkyl. As will be appreciated by thoseskilled in the art, Ziegler-Natta catalyst systems may containadditional components; a non-limiting example of an additional componentis an electron donor, e.g. amines or ethers.

A non-limiting example of an active in-line (or batch) Ziegler-Nattacatalyst system can be prepared as follows. In the first step, asolution of a magnesium compound is reacted with a solution of achloride compound to form a magnesium chloride support suspended insolution. Non-limiting examples of magnesium compounds include Mg(R¹)₂;wherein the R¹ groups may be the same or different, linear, branched orcyclic hydrocarbyl radicals containing 1 to 10 carbon atoms.Non-limiting examples of chloride compounds include R²Cl; wherein R²represents a hydrogen atom, or a linear, branched or cyclic hydrocarbylradical containing 1 to 10 carbon atoms. In the first step, the solutionof magnesium compound may also contain an aluminum alkyl. Non-limitingexamples of aluminum alkyl include Al(R³)₃, wherein the R³ groups may bethe same or different, linear, branched or cyclic hydrocarbyl radicalscontaining from 1 to 10 carbon atoms. In the second step a solution ofthe metal compound is added to the solution of magnesium chloride andthe metal compound is supported on the magnesium chloride. Non-limitingexamples of suitable metal compounds include M(X)_(n) or MO(X)_(n);where M represents a metal chosen from Group 4 through Group 8 of thePeriodic Table, or mixtures of metals chosen from Group 4 through Group8; O represents oxygen, and; X represents chloride or bromide; n is aninteger from 3 to 6 that satisfies the oxidation state of the metal.Additional non-limiting examples of suitable metal compounds includeGroup 4 to Group 8 metal alkyls, metal alkoxides (which may be preparedby reacting a metal alkyl with an alcohol) and mixed-ligand metalcompounds that contain a mixture of halide, alkyl and alkoxide ligands.In the third step a solution of an alkyl aluminum co-catalyst is addedto the metal compound supported on the magnesium chloride. A widevariety of alkyl aluminum co-catalysts are suitable, as expressed byformula:

Al(R⁴)_(p)(OR⁹)_(q)(X)_(r)

wherein the R⁴ groups may be the same or different, hydrocarbyl groupshaving from 1 to 10 carbon atoms; the OR⁹ groups may be the same ordifferent, alkoxy or aryloxy groups wherein R⁹ is a hydrocarbyl grouphaving from 1 to 10 carbon atoms bonded to oxygen; X is chloride orbromide, and; (p+q+r)=3, with the proviso that p is greater than 0.Non-limiting examples of commonly used alkyl aluminum co-catalystsinclude trimethyl aluminum, triethyl aluminum, tributyl aluminum,dimethyl aluminum methoxide, diethyl aluminum ethoxide, dibutyl aluminumbutoxide, dimethyl aluminum chloride or bromide, diethyl aluminumchloride or bromide, dibutyl aluminum chloride or bromide and ethylaluminum dichloride or dibromide.

The process described in the paragraph above, to synthesize an activein-line (or batch) Ziegler-Natta catalyst system, can be carried out ina variety of solvents; non-limiting examples of solvents include linearor branched C₅ to C₁₂ alkanes or mixtures thereof.

In an embodiment of the disclosure, the third polyethylene is anethylene copolymer. Suitable alpha-olefins which may be copolymerizedwith ethylene to give the third polyethylene include 1-propene,1-butene, 1-pentene, 1-hexene and 1-octene.

In an embodiment of the disclosure, the third polyethylene is anethylene homopolymer.

In an embodiment of the disclosure, the third polyethylene is aheterogeneously branched ethylene copolymer.

In an embodiment of the disclosure, the third polyethylene is anethylene/I-octene copolymer.

In embodiments of the disclosure, the third polyethylene has a molecularweight distribution, M_(w)/M_(n) of ≥2.3, or ≥2.3, or ≥2.5, or ≥2.5, or≥2.7, or ≥2.7, or ≥2.9, or ≥2.9, or ≥3.0, or 3.0. In embodiments of thedisclosure, the third polyethylene has a molecular weight distribution,M_(w)/M_(n) of from 2.3 to 6.5, or from 2.3 to 6.0, or from 2.3 to 5.5,or from 2.3 to 5.0, or from 2.3 to 4.5, or from 2.3 to 4.0, or from 2.5to 6.0, or from 2.5 to 5.5, or from 2.5 to 5.0, or from 2.5 to 4.5, orfrom 2.5 to 4.0, or from 2.7 to 6.0, or from 2.7 to 5.5, or from 2.7 to5.0, or from 2.7 to 4.5, or from 2.9 to 6.5, or from 2.9 to 6.0, or from2.9 to 5.5, or from 2.9 to 5.0, or from 2.9 to 4.5.

In an embodiment of the disclosure, the third polyethylene has from 0 to100 short chain branches per thousand carbon atoms (SCB_(PE-3)). Infurther embodiments, the third polyethylene has from 0 to 50 short chainbranches per thousand carbon atoms (SCB_(PE-3)), or from 0 to 35 shortchain branches per thousand carbon atoms (SCB_(PE-3)), or from 3 to 30short chain branches per thousand carbon atoms (SCB_(PE-3)), or from 5to 30 short chain branches per thousand carbon atoms (SCB_(PE-3)), orfrom 5 to 25 short chain branches per thousand carbon atoms(SCB_(PE-3)), or from 3 to 25 short chain branches per thousand carbonatoms (SCB_(PE-3)), or from 1 to 25 short chain branches per thousandcarbon atoms (SCB_(PE-3)), or from 0.1 to 20 short chain branches perthousand carbon atoms (SCB_(PE-3)).

The short chain branching (i.e. the short chain branching per thousandcarbons, SCB_(PE-3)), if present, is the branching due to the presenceof alpha-olefin comonomer in the polethylene and will for example havetwo carbon atoms for a 1-butene comonomer, or four carbon atoms for a1-hexene comonomer, or six carbon atoms for a 1-octene comonomer, etc.

In an embodiment of the disclosure, the number of short chain branchesper thousand carbon atoms in the third polyethylene (SCB_(PE-3)) isgreater than the number of short chain branches per thousand carbonatoms in the second polyethylene (SCB_(PE-2)).

In embodiments of the disclosure, the upper limit on the density, d3 ofthe third polyethylene may be about 0.975 g/cm³; in some cases, about0.965 g/cm³ and; in other cases, about 0.955 g/cm³. In embodiments ofthe disclosure, the lower limit on the density, d3 of the thirdpolyethylene may be about 0.855 g/cm³, in some cases about 0.865 g/cm³,and; in other cases, about 0.875 g/cm³.

In embodiments of the disclosure the density, d3 of the thirdpolyethylene may be from about 0.875 g/cm³ to about 0.965 g/cm³, or fromabout 0.875 g/cm³ to about 0.960 g/cm³, or from about 0.875 g/cm³ to0.950 g/cm³, or from about 0.865 g/cm³ to about 0.940 g/cm³, or fromabout 0.865 g/cm³ to about 0.936 g/cm³, or from about 0.865 g/cm³ toabout 0.932 g/cm³, or from about 0.865 g/cm³ to about 0.926 g/cm³, orfrom about 0.865 g/cm³ to about 0.921 g/cm³, or from about 0.865 g/cm³to about 0.918 g/cm³, or from about 0.875 g/cm³ to about 0.916 g/cm³, orfrom about 0.875 g/cm³ to about 0.916 g/cm³, or from about 0.865 g/cm³to about 0.912 g/cm³, or from about 0.880 g/cm³ to about 0.912 g/cm³, orfrom about 0.890 g/cm³ to about 0.916 g/cm³, or from about 0.900 g/cm³to about 0.916 g/cm³, or from about 0.880 g/cm³ to about 0.916 g/cm³, orfrom about 0.880 g/cm³ to about 0.918 g/cm³, or from about 0.880 g/cm³to about 0.921 g/cm³, or from about 0.880 g/cm³ to about 0.926 g/cm³, orfrom about 0.880 g/cm³ to about 0.932 g/cm³, or from about 0.880 g/cm³to about 0.936 g/cm³.

In an embodiment of the disclosure, the third polyethylene is anethylene copolymer which has a composition distribution breadth index,CDBI₅₀ of 75 wt. % or less, or 70 wt. % or less. In further embodimentsof the disclosure, the third polyethylene is an ethylene copolymer whichhas a CDBI₅₀ of 65 wt. % or less, or 60 wt. % or less, or 55 wt. % orless, or 50 wt. % or less, or 45 wt. % or less.

In embodiments of the disclosure the melt index of the thirdpolyethylene I₂ ³ may be from about 0.01 dg/min to about 1000 dg/min, orfrom about 0.01 dg/min to about 500 dg/min, or from about 0.01 dg/min toabout 100 dg/min, or from about 0.01 dg/min to about 50 dg/min, or fromabout 0.01 dg/min to about 25 dg/min, or from about 0.01 dg/min to about10 dg/min, or from about 0.01 dg/min to about 5 dg/min, or from about0.01 dg/min to about 3 dg/min, or from about 0.01 dg/min to about 1dg/min, or less than about 5 dg/min, or less than about 3 dg/min, orless than about 1.0 dg/min, or less than about 0.75 dg/min, or less thanabout 0.50 dg/min.

In an embodiment of the disclosure, the third polyethylene has a weightaverage molecular weight, M_(w) of from about 50,000 to about 300,000,or from about 50,000 to about 250,000, or from about 60,000 to about250,000, or from about 70,000 to about 250,000, or from about 75,000 toabout 200,000, or from about 80,000 to about 275,000; or from about80,000 to about 250,000, or from about 80,000 to about 200,000, or from70,000 to about 200,000, or from about 80,000 to about 175,000.

In an embodiment of the disclosure, the third polyethylene has a weightaverage molecular weight, M_(w) which is greater than the weight averagemolecular weight, M_(w) of the first polyethylene.

In an embodiment of the disclosure, the third polyethylene has a weightaverage molecular weight, M_(w) which is greater than the weight averagemolecular weight, M_(w) of the second polyethylene.

In embodiments of the disclosure, the upper limit on the weight percent(wt. %) of the third polyethylene in the polyethylene composition (i.e.the weight percent of the third polyethylene based on the total weightof the first, the second and the third polyethylene) may be about 90 wt.%, or about 85 wt. %, or about 80 wt. %, or about 75 wt. %, or 65 wt. %,in other cases about 60 wt. %, in other cases about 55 wt. %, or about50 wt. %, or about 45 wt. %. In embodiments of the disclosure, the lowerlimit on the wt. % of the third polyethylene in the final polyethyleneproduct may be about 5 wt. %, or about 10 wt. %, or about 15 wt. %, orabout 20 wt. %, or about 25 wt. %, or about 30 wt. %, or about 35 wt. %,or in other cases about 40 wt. %.

In an embodiments of the disclosure, third polyethylene has no longchain branching present or does not have any detectable levels of longchain branching.

The Polyethylene Composition

The polyethylene compositions disclosed herein can be made using anywell-known techniques in the art, including but not limited to meltblending, solution blending, or in-reactor blending to bring together afirst polyethylene, a second polyethylene and a third polyethylene.

In an embodiment, the polyethylene composition of the present disclosureis made by melt blending or solution blending three differentpolyethylene components: i) a first polyethylene, ii) a secondpolyethylene, and iii) a third polyethylene.

In an embodiment, the polyethylene composition of the present disclosureis made by melt blending or solution blending two different polyethylenecomponents: i) a first polyethylene component including a firstpolyethylene and a second polyethylene, and ii) second polyethylenecomponent including a third polyethylene.

In an embodiment, the polyethylene composition of the present disclosureis made by melt blending or solution blending two different polyethylenecomponents: i) a first polyethylene component including a firstpolyethylene and ii) a second polyethylene component including a secondpolyethylene and a third polyethylene.

In an embodiment, the polyethylene composition of the present disclosureis made by melt blending or solution blending two different polyethylenecomponents: i) a first polyethylene component including a firstpolyethylene and a third polyethylene, and ii) a second polyethylenecomponent including a second polyethylene.

In an embodiment, the polyethylene composition of the present disclosureis made using the same single site catalyst in two different reactors,where each reactor is operated under different polymerization conditionsto give a first polyethylene and a second polyethylene and using amulti-site catalyst in another reactor to give the third polyethylene.

In an embodiment, the polyethylene composition of the present disclosureis made using a different single site catalyst in two differentreactors, where each reactor is operated under similar or differentpolymerization conditions to give a first polyethylene and a secondpolyethylene, and using a multi-site catalyst in another reactor to givethe third polyethylene.

It is also contemplated by the present disclosure, that the polymercompositions including a first, second and third polyethylene could bemade in one or more polymerization reactor, using two different singlesite polymerization catalysts and a multi-site polymerization catalyst,where each catalyst has a different response to one or more of hydrogenconcentration, ethylene concentration, comonomer concentration, andtemperature under a given set of polymerization conditions, so that thefirst polyethylene is produced by the first single site catalyst, thesecond polyethylene is produced by the second single site catalyst, andthe third polyethylene is produced by the multi-site catalyst.

It is also contemplated by the present disclosure, that the polymercompositions including a first, second and third polyethylene could bemade in one or more polymerization reactors, using one or more singlesite polymerization catalysts, and one multi-site catalyst, where eachcatalyst has a similar or different response to one or more of hydrogenconcentration, ethylene concentration, comonomer concentration, andtemperature under a given set of polymerization conditions, and whereone or more of hydrogen concentration, ethylene concentration, comonomerconcentration, and temperature are cycled through a range so that afirst, second and a third polyethylene is produced by the one or moresingle site catalysts and the one multi-site catalyst present in the oneor more polymerization reactors.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first reactor bypolymerizing ethylene and an alpha olefin with a single site catalyst;forming a second polyethylene in a second reactor by polymerizingethylene and optionally an alpha olefin with a single site catalyst, andforming a third polyethylene in a third reactor by polymerizing ethyleneand optionally an alpha olefin with a multi-site catalyst.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first reactor bypolymerizing ethylene and an alpha olefin with a single site catalyst;forming a second polyethylene in a second reactor by polymerizingethylene and optionally an alpha olefin with a single site catalyst, andforming a third polyethylene in a third reactor by polymerizing ethyleneand optionally an alpha olefin with a multi-site catalyst, where atleast two of the first, second and third reactors are configured inseries with one another.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first solution phasepolymerization reactor by polymerizing ethylene and an alpha olefin witha single site catalyst; forming a second polyethylene in a secondsolution phase polymerization reactor by polymerizing ethylene andoptionally an alpha olefin with a single site catalyst, and forming athird polyethylene in a third solution phase polymerization reactor bypolymerizing ethylene and optionally an alpha olefin with a multi-sitecatalyst.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first solution phasepolymerization reactor by polymerizing ethylene and an alpha olefin witha single site catalyst; forming a second polyethylene in a secondsolution phase polymerization reactor by polymerizing ethylene andoptionally an alpha olefin with a single site catalyst, and forming athird polyethylene in a third solution phase polymerization reactor bypolymerizing ethylene and optionally an alpha olefin with a multi-sitecatalyst, where at least two of the first, second and third solutionphase polymerization reactors are configured in series with one another.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first solution phasepolymerization reactor by polymerizing ethylene and an alpha olefin witha single site catalyst; forming a second polyethylene in a secondsolution phase polymerization reactor by polymerizing ethylene andoptionally an alpha olefin with a single site catalyst, and forming athird polyethylene in a third solution phase polymerization reactor bypolymerizing ethylene and optionally an alpha olefin with a multi-sitecatalyst, where the first and second solution phase polymerizationreactors are configured in series with one another.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first reactor bypolymerizing ethylene and an alpha olefin with a single site catalyst;forming a second polyethylene in a second reactor by polymerizingethylene and optionally an alpha olefin with a single site catalyst, andforming a third polyethylene in a third reactor by polymerizing ethyleneand optionally an alpha olefin with a multi-site catalyst, where each ofthe first, second and third reactors are configured in parallel to oneanother.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first solution phasepolymerization reactor by polymerizing ethylene and an alpha olefin witha single site catalyst; forming a second polyethylene in a secondsolution phase polymerization reactor by polymerizing ethylene andoptionally an alpha olefin with a single site catalyst, and forming athird polyethylene in a third solution phase polymerization reactor bypolymerizing ethylene and optionally an alpha olefin with a multi-sitecatalyst, where each of the first, second and third solution phasepolymerization reactors are configured in parallel to one another.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first reactor bypolymerizing ethylene and an alpha olefin with a single site catalyst;forming a second polyethylene in a second reactor by polymerizingethylene and optionally an alpha olefin with a single site catalyst, andforming a third polyethylene in a third reactor by polymerizing ethyleneand optionally an alpha olefin with a multi-site catalyst, where thefirst and second reactors are configured in series to one another, andthe third reactor is configured in parallel to the first and secondreactors.

In an embodiment, the polyethylene composition of the present disclosureis made by forming a first polyethylene in a first solution phasereactor by polymerizing ethylene and an alpha olefin with a single sitecatalyst; forming a second polyethylene in a second solution phasereactor by polymerizing ethylene and optionally an alpha olefin with asingle site catalyst, and forming a third polyethylene in a thirdsolution phase reactor by polymerizing ethylene and optionally an alphaolefin with a multi-site catalyst, where the first and second solutionphase reactors are configured in series to one another, and the thirdsolution phase reactor is configured in parallel to the first and secondreactors.

In an embodiment, the solution phase polymerization reactor used as afirst solution phase reactor, a second solution phase reactor, or athird solution phase reactor is a continuously stirred tank reactor.

In an embodiment, the solution phase polymerization reactor used as afirst solution phase reactor, a second solution phase reactor, or athird solution phase reactor is a tubular reactor.

In a solution phase polymerization reactor, a variety of solvents may beused as the process solvent; non-limiting examples include linear,branched or cyclic C₅ to C₁₂ alkanes. Non-limiting examples of α-olefinsinclude 1-propene, 1-butene, 1-pentene, 1-hexene and 1-octene. Suitablecatalyst component solvents include aliphatic and aromatic hydrocarbons.Non-limiting examples of aliphatic catalyst component solvents includelinear, branched or cyclic C₅-12 aliphatic hydrocarbons, e.g. pentane,methyl pentane, hexane, heptane, octane, cyclohexane, cyclopentane,methylcyclohexane, hydrogenated naphtha or combinations thereof.Non-limiting examples of aromatic catalyst component solvents includebenzene, toluene (methylbenzene), ethylbenzene, o-xylene(1,2-dimethylbenzene), m-xylene (1,3-dimethylbenzene), p-xylene(1,4-dimethylbenzene), mixtures of xylene isomers, hemellitene(1,2,3-trimethylbenzene), pseudocumene (1,2,4-trimethylbenzene),mesitylene (1,3,5-trimethylbenzene), mixtures of trimethylbenzeneisomers, prehenitene (1,2,3,4-tetramethylbenzene), durene(1,2,3,5-tetramethylbenzene), mixtures of tetramethylbenzene isomers,pentamethylbenzene, hexamethylbenzene and combinations thereof.

In embodiments of the disclosure, the polyethylene composition has adensity which may be from about 0.880 g/cm³ to about 0.965 g/cm³, orfrom about 0.885 g/cm³ to about 0.960 g/cm³, or from about 0.890 g/cm³to 0.950 g/cm³, or from about 0.895 g/cm³ to about 0.940 g/cm³, or fromabout 0.900 g/cm³ to about 0.936 g/cm³, or from about 0.905 g/cm³ toabout 0.934 g/cm³, or from about 0.910 g/cm³ to about 0.932 g/cm³, orfrom about 0.910 g/cm³ to about 0.930 g/cm³, or from about 0.910 g/cm³to about 0.926 g/cm³, or from about 0.890 g/cm³ to about 0.924 g/cm³, orfrom about 0.890 g/cm³ to about 0.922 g/cm³, or from about 0.890 g/cm³to about 0.920 g/cm³, or from about 0.890 g/cm³ to about 0.918 g/cm³, orfrom about 0.880 g/cm³ to about 0.922 g/cm³, or from about 0.880 g/cm³to about 0.926 g/cm³, or from about 0.880 g/cm³ to about 0.932 g/cm³, or≤0.948 g/cm³, or <0.948 g/cm³, or ≤0.945 g/cm³, or <0.945 g/cm³, or≤0.940 g/cm³, or <0.940 g/cm³, or ≤0.939 g/cm³, or <0.939 g/cm³, or≤0.935 g/cm³, or <0.935 g/cm³, or ≤0.932 g/cm³, or <0.932 g/cm³.

In embodiments of the disclosure the melt index I₂ of the polyethylenecomposition may be from about 0.01 dg/min to about 1000 dg/min, or fromabout 0.01 dg/min to about 500 dg/min, or from about 0.01 dg/min toabout 100 dg/min, or from about 0.01 dg/min to about 50 dg/min, or fromabout 0.01 dg/min to about 25 dg/min, or from about 0.01 dg/min to about10 dg/min, or from about 0.01 dg/min to about 5 dg/min, or from about0.01 dg/min to about 3 dg/min, or from about 0.01 dg/min to about 1dg/min, or from about 0.1 dg/min to about 10 dg/min, or from about 0.1dg/min to about 5 dg/min, or from about 0.1 dg/min to about 3 dg/min, orfrom about 0.1 dg/min to about 2 dg/min, or from about 0.1 dg/min toabout 1.5 dg/min, or from about 0.1 dg/min to about 1 dg/min, or lessthan about 5 dg/min, or less than about 3 dg/min, or less than about 1.0dg/min.

In embodiments of the disclosure the high load melt index I₂₁ of thepolyethylene composition may be from about 15 dg/min to about 10,000dg/min, or from about 15 dg/min to about 1000 dg/min, or from about 15dg/min to about 100 dg/min, or from about 15 dg/min to about 75 dg/min,or from about 15 dg/min to about 50 dg/min, or from about 10 dg/min toabout 100 dg/min, or from about 10 dg/min to about 75 dg/min, or fromabout 10 dg/min to about 50 dg/min, or from about 10 dg/min to about 45dg/min, or from about 10 dg/min to about 40 dg/min, or from about 10dg/min to about 35 dg/min, or from about 10 dg/min to about 32 dg/min,or from about 10 dg/min to about 36 dg/min.

In an embodiment of the disclosure the melt flow ratio I₂₁/I₂ of thepolyethylene composition is ≤40. In embodiments of the disclosure themelt flow ratio I₂₁/I₂ of the polyethylene composition may be from about15 to about 40, or from about 15 to about 38, or from about 18 to about40, or from about 20 to about 40, or from about 25 to about 40, or fromabout 28 to about 40.

In an embodiments of the disclosure, the polyethylene composition has aweight average molecular weight, M_(w) of from about 50,000 to about300,000, or from about 50,000 to about 250,000, or from about 60,000 toabout 250,000, or from about 70,000 to about 225,000, or from about70,000 to about 200,000, or from about 75,000 to about 175,000, or fromabout 75,000 to about 150,000, or from about 100,000 to about 130,000.

In embodiments of the disclosure, the polyethylene composition has alower limit molecular weight distribution, M_(w)/M_(n) of 2.0, or 2.1,or 2.3, or 2.5. In embodiments of the disclosure, the polyethylenecomposition has an upper limit molecular weight distribution,M_(w)/M_(n) of 6.0, or 5.5, or 5.0, or 4.5, or 4.0, or 3.5, or 3.0. Inembodiments of the disclosure, the polyethylene composition has amolecular weight distribution, M_(w)/M_(n) of from 2.1 to 6.0, or from2.3 to 6.0, or from 2.5 to 6.0, or from 2.1 to 5.5, or from 2.3 to 5.5,or from 2.1 to 5.0, or from 2.3 to 5.0, or from 2.1 to 4.5, or from 2.3to 4.5, or from 2.1 to 4.0, or from 2.3 to 4.0, or from 2.1 to 3.5, orfrom 2.3 to 3.5, or from 2.1 to 3.0, or from 2.3 to 3.0.

In embodiments of the disclosure, the polyethylene composition has aZ-average molecular weight distribution, M_(Z)/M_(W) of ≤4.0, or <4.0,or ≤3.5, or <3.5, or ≤3.0, or <3.0, or ≤2.75, or <2.75, or ≤2.50, or<2.50. In embodiments of the disclosure, the polyethylene compositionhas a Z-average molecular weight distribution, M_(Z)/M_(W) of from 1.5to 4.0, or from 1.75 to 3.5, or from 1.75 to 3.0, or from 2.0 to 4.0, orfrom 2.0 to 3.5, or from 2.0 to 3.0, or from 2.0 to 2.5.

In an embodiment of the disclosure, the polyethylene composition has aunimodal profile in a gel permeation chromatograph generated accordingto the method of ASTM D6474-99. The term “unimodal” is herein defined tomean there will be only one significant peak or maximum evident in theGPC-curve. A unimodal profile includes a broad unimodal profile. Incontrast, the use of the term “bimodal” is meant to convey that inaddition to a first peak, there will be a secondary peak or shoulderwhich represents a higher or lower molecular weight component (i.e. themolecular weight distribution, can be said to have two maxima in amolecular weight distribution curve). Alternatively, the term “bimodal”connotes the presence of two maxima in a molecular weight distributioncurve generated according to the method of ASTM D6474-99. The term“multi-modal” denotes the presence of two or more, typically more thantwo, maxima in a molecular weight distribution curve generated accordingto the method of ASTM D6474-99.

In an embodiment of the disclosure the polyethylene composition may havea multimodal profile in a differential scanning calorimetry (DSC) graph.In the context of DSC analysis, the term “multimodal” connotes a DSCprofile in which two or more distinct melting peaks are observable.

In an embodiment of the disclosure the polyethylene composition may havea bimodal profile in a differential scanning calorimetry (DSC) graph. Inthe context of DSC analysis, the term “bimodal” connotes a DSC profilein which two distinct melting peaks are observable.

In an embodiment of the disclosure, the polyethylene composition has amelting peak temperature in a differential scanning calorimetry (DSC)analysis at above 120° C. For clarity sake, by the phrase “has a meltingpeak temperature in an DSC analysis” it is meant that in a DSC analysis,although there may be one or more melting peaks evident, at least onesuch peak occurs at above the indicated temperature. In an embodiment ofthe disclosure, the polyethylene composition has a melting peaktemperature in a differential scanning calorimetry (DSC) analysis atabove 123° C. In an embodiment of the disclosure, the polyethylenecomposition has a melting peak temperature in a differential scanningcalorimetry (DSC) analysis at above 125° C.

In an embodiment of the disclosure, the polyethylene composition willhave a reverse or partially reverse comonomer distribution profile asmeasured using GPC-FTIR. If the comonomer incorporation decreases withmolecular weight, as measured using GPC-FTIR, the distribution isdescribed as “normal”. If the comonomer incorporation is approximatelyconstant with molecular weight, as measured using GPC-FTIR, thecomonomer distribution is described as “flat” or “uniform”. The terms“reverse comonomer distribution” and “partially reverse comonomerdistribution” mean that in the GPC-FTIR data obtained for a copolymer,there is one or more higher molecular weight components having a highercomonomer incorporation than in one or more lower molecular weightcomponents. The term “reverse(d) comonomer distribution” is used hereinto mean, that across the molecular weight range of an ethylenecopolymer, comonomer contents for the various polymer fractions are notsubstantially uniform and the higher molecular weight fractions thereofhave proportionally higher comonomer contents (i.e. if the comonomerincorporation rises with molecular weight, the distribution is describedas “reverse” or “reversed”). Where the comonomer incorporation riseswith increasing molecular weight and then declines, the comonomerdistribution is still considered “reverse”, but may also be described as“partially reverse”. A partially reverse comonomer distribution willexhibit a peak or maximum.

In an embodiment of the disclosure the polyethylene composition has areversed comonomer distribution profile as measured using GPC-FTIR.

In an embodiment of the disclosure the polyethylene composition has apartially reversed comonomer distribution profile as measured usingGPC-FTIR.

In an embodiment of the disclosure, the polyethylene composition has asoluble fraction of at least 10 wt. % in a crystallization elutionfractionation (CEF) analysis, where the soluble fraction is defined asthe weight percent (wt. %) of material which elutes at 30° C. and below.In an embodiment of the disclosure, the polyethylene composition has asoluble fraction of at least 15 wt. % in a crystallization elutionfractionation (CEF) analysis, where the soluble fraction is defined asthe weight percent (wt. %) of material which elutes at 30° C. and below.In an embodiment of the disclosure, the polyethylene composition has asoluble fraction of at least 17 wt. % in a crystallization elutionfractionation (CEF) analysis, where the soluble fraction is defined asthe weight percent (wt. %) of material which elutes at 30° C. and below.In an embodiment of the disclosure, the polyethylene composition has asoluble fraction of at least 20 wt. % in a crystallization elutionfractionation (CEF) analysis, where the soluble fraction is defined asthe weight percent (wt. %) of material which elutes at 30° C. and below.In an embodiment of the disclosure, the polyethylene composition has asoluble fraction of at least 25 wt. % in a crystallization elutionfractionation (CEF) analysis, where the soluble fraction is defined asthe weight percent (wt. %) of material which elutes at 30° C. and below.In an embodiment of the disclosure, the polyethylene composition has asoluble fraction of from 10 to 40 wt. % in a crystallization elutionfractionation (CEF) analysis, where the soluble fraction is defined asthe weight percent (wt. %) of material which elutes at 30° C. and below.In an embodiment of the disclosure, the polyethylene composition has asoluble fraction of from 15 to 35 wt. % in a crystallization elutionfractionation (CEF) analysis, where the soluble fraction is defined asthe weight percent (wt. %) of material which elutes at 30° C. and below.

In an embodiment of the disclosure, the polyethylene composition has astress exponent, defined as Log₁₀[I₆/I₂]/Log₁₀[6.48/2.16], which is≤1.50. In further embodiments of the disclosure the polyethylenecomposition has a stress exponent, Log₁₀[1 ₆/I₂]/Log₁₀[6.48/2.16] ofless than 1.48, or less than 1.45, or less than 1.43.

In an embodiment of the disclosure, the polyethylene composition has ahexane extractable value of ≤5.0 weight percent, or less than 4.0 wt. %,or less than 3.0 wt. %, or less than 2.0 wt. %, or less than 1.0 wt. %.

The polyethylene composition disclosed herein may be converted intoflexible manufactured articles such as monolayer or multilayer films,such films are well known to those experienced in the art; non-limitingexamples of processes to prepare such films include blown film and castfilm processes.

In the blown film extrusion process an extruder heats, melts, mixes andconveys a thermoplastic, or a thermoplastic blend. Once molten, thethermoplastic is forced through an annular die to produce athermoplastic tube. In the case of co-extrusion, multiple extruders areemployed to produce a multilayer thermoplastic tube. The temperature ofthe extrusion process is primarily determined by the thermoplastic orthermoplastic blend being processed, for example the melting temperatureor glass transition temperature of the thermoplastic and the desiredviscosity of the melt. In the case of polyolefins, typical extrusiontemperatures are from 330° F. to 550° F. (166° C. to 288° C.). Upon exitfrom the annular die, the thermoplastic tube is inflated with air,cooled, solidified and pulled through a pair of nip rollers. Due to airinflation, the tube increases in diameter forming a bubble of desiredsize. Due to the pulling action of the nip rollers the bubble isstretched in the machine direction. Thus, the bubble is stretched in twodirections: the transverse direction (TD) where the inflating airincreases the diameter of the bubble; and the machine direction (MD)where the nip rollers stretch the bubble. As a result, the physicalproperties of blown films are typically anisotropic, i.e. the physicalproperties differ in the MD and TD directions; for example, film tearstrength and tensile properties typically differ in the MD and TD. Insome references, the terms “cross direction” or “CD” is used; theseterms are equivalent to the terms “transverse direction” or “TD” used inthis disclosure. In the blown film process, air is also blown on theexternal bubble circumference to cool the thermoplastic as it exits theannular die. The final width of the film is determined by controllingthe inflating air or the internal bubble pressure; in other words,increasing or decreasing bubble diameter. Film thickness is controlledprimarily by increasing or decreasing the speed of the nip rollers tocontrol the draw-down rate. After exiting the nip rollers, the bubble ortube is collapsed and may be slit in the machine direction thus creatingsheeting. Each sheet may be wound into a roll of film. Each roll may befurther slit to create film of the desired width. Each roll of film isfurther processed into a variety of consumer products as describedbelow.

The cast film process is similar in that a single or multipleextruder(s) may be used; however the various thermoplastic materials aremetered into a flat die and extruded into a monolayer or multilayersheet, rather than a tube. In the cast film process the extruded sheetis solidified on a chill roll.

Depending on the end-use application, the disclosed polyethylenecomposition may be converted into films that span a wide range ofthicknesses. Non-limiting examples include, food packaging films wherethicknesses may range from about 0.5 mil (13 μm) to about 4 mil (102μm), and; in heavy duty sack applications film thickness may range fromabout 2 mil (51 μm) to about 10 mil (254 μm).

The polyethylene composition disclosed herein may be used in monolayerfilms; where the monolayer may contain more than one polyethylenecomposition and/or additional thermoplastics; non-limiting examples ofthermoplastics include polyethylene polymers and propylene polymers. Thelower limit on the weight percent of the polyethylene composition in amonolayer film may be about 3 wt. %, in other cases about 10 wt. % andin still other cases about 30 wt. %. The upper limit on the weightpercent of the polyethylene composition in the monolayer film may be 100wt. %, in other cases about 90 wt. % and in still other cases about 70wt. %.

The polyethylene composition disclosed herein may also be used in one ormore layers of a multilayer film; non-limiting examples of multilayerfilms include three, five, seven, nine, eleven or more layers. Thethickness of a specific layer (containing the polyethylene composition)within a multilayer film may be about 5%, in other cases about 15% andin still other cases about 30% of the total multilayer film thickness.In other embodiments, the thickness of a specific layer (containing thepolyethylene composition) within a multilayer film may be about 95%, inother cases about 80% and in still other cases about 65% of the totalmultilayer film thickness. Each individual layer of a multilayer filmmay contain more than one polyethylene composition and/or additionalthermoplastics.

Additional embodiments include laminations and coatings, wherein mono ormultilayer films containing the disclosed polyethylene composition areextrusion laminated or adhesively laminated or extrusion coated. Inextrusion lamination or adhesive lamination, two or more substrates arebonded together with a thermoplastic or an adhesive, respectively. Inextrusion coating, a thermoplastic is applied to the surface of asubstrate. These processes are well known to those experienced in theart. Frequently, adhesive lamination or extrusion lamination are used tobond dissimilar materials, non-limiting examples include the bonding ofa paper web to a thermoplastic web, or the bonding of an aluminum foilcontaining web to a thermoplastic web, or the bonding of twothermoplastic webs that are chemically incompatible, e.g. the bonding ofa polyethylene composition containing web to a polyester or polyamideweb. Prior to lamination, the web containing the disclosed polyethylenecomposition(s) may be monolayer or multilayer. Prior to lamination theindividual webs may be surface treated to improve the bonding, anon-limiting example of a surface treatment is corona treating. Aprimary web or film may be laminated on its upper surface, its lowersurface, or both its upper and lower surfaces with a secondary web. Asecondary web and a tertiary web could be laminated to the primary web;wherein the secondary and tertiary webs differ in chemical composition.As non-limiting examples, secondary or tertiary webs may include;polyamide, polyester and polypropylene, or webs containing barrier resinlayers such as EVOH. Such webs may also contain a vapor depositedbarrier layer; for example, a thin silicon oxide (SiO_(x)) or aluminumoxide (AlO_(x)) layer. Multilayer webs (or films) may contain three,five, seven, nine, eleven or more layers.

The polyethylene composition disclosed herein can be used in a widerange of manufactured articles including one or more films or filmlayers (monolayer or multilayer). Non-limiting examples of suchmanufactured articles include: food packaging films (fresh and frozenfoods, liquids and granular foods), stand-up pouches, retortablepackaging and bag-in-box packaging; barrier films (oxygen, moisture,aroma, oil, etc.) and modified atmosphere packaging; light and heavyduty shrink films and wraps, collation shrink film, pallet shrink film,shrink bags, shrink bundling and shrink shrouds; light and heavy dutystretch films, hand stretch wrap, machine stretch wrap and stretch hoodfilms; high clarity films; heavy-duty sacks; household wrap, overwrapfilms and sandwich bags; industrial and institutional films, trash bags,can liners, magazine overwrap, newspaper bags, mail bags, sacks andenvelopes, bubble wrap, carpet film, furniture bags, garment bags, coinbags, auto panel films; medical applications such as gowns, draping andsurgical garb; construction films and sheeting, asphalt films,insulation bags, masking film, landscaping film and bags; geomembraneliners for municipal waste disposal and mining applications; batchinclusion bags; agricultural films, mulch film and green house films;in-store packaging, self-service bags, boutique bags, grocery bags,carry-out sacks and t-shirt bags; oriented films, machine direction andbiaxially oriented films and functional film layers in orientedpolypropylene (OPP) films, e.g. sealant and/or toughness layers.Additional manufactured articles including one or more films containingat least one polyethylene composition include laminates and/ormultilayer films; sealants and tie layers in multilayer films andcomposites; laminations with paper; aluminum foil laminates or laminatescontaining vacuum deposited aluminum; polyamide laminates; polyesterlaminates; extrusion coated laminates, and; hot-melt adhesiveformulations. The manufactured articles summarized in this paragraphcontain at least one film (monolayer or multilayer) including at leastone embodiment of the disclosed polyethylene composition.

Desired film physical properties (monolayer or multilayer) typicallydepend on the application of interest. Non-limiting examples ofdesirable film properties include: optical properties (gloss, haze andclarity), dart impact, Elmendorf tear, modulus (1% and 2% secantmodulus), puncture-propagation tear resistance, tensile properties(yield strength, break strength, elongation at break, toughness, etc.)and heat sealing properties (heat seal initiation temperature and hottack strength). Specific hot tack and heat sealing properties aredesired in high speed vertical and horizontal form-fill-seal processesthat load and seal a commercial product (liquid, solid, paste, part,etc.) inside a pouch-like package.

In addition to desired film physical properties, it is desired that thedisclosed polyethylene composition is easy to process on film lines.Those skilled in the art frequently use the term “processability” todifferentiate polymers with improved processability, relative topolymers with inferior processability. A commonly used measure toquantify processability is extrusion pressure; for example, a polymerwith improved processability has a lower extrusion pressure (on a blownfilm or a cast film extrusion line) relative to a polymer with inferiorprocessability.

In an embodiment of the disclosure, a film or film layer includes thepolyethylene composition described above.

In embodiments of the disclosure, a film or film layer includes thepolyethylene composition described above and has a thickness of from 0.5to 10 mil.

In embodiments of the disclosure, a film or film layer has a thicknessof from 0.5 to 10 mil.

In embodiments of the disclosure, a film will have a dart impactstrength of ≥400 g/mil, or ≥450 g/mil, or ≥500 g/mil, or ≥600 g/mil, or≥700 g/mil. In another embodiment of the disclosure, a film will have adart impact strength of from 400 g/mil to 950 g/mil. In a furtherembodiment of the disclosure, a film will have dart impact strength offrom 400 g/mil to 850 g/mil. In a further embodiment of the disclosure,a film will have dart impact strength of from 500 g/mil to 900 g/mil. Ina further embodiment of the disclosure, a film will have dart impactstrength of from 550 g/mil to 850 g/mil. In yet another embodiment ofthe disclosure, the film will have dart impact strength of from 600g/mil to 850 g/mil. In still yet another embodiment of the disclosure, afilm will have dart impact strength of from 600 g/mil to 800 g/mil.

In embodiments of the disclosure, a 1 mil film will have a machinedirection (MD) secant modulus at 1% strain of ≥150 MPa, or ≥160 MPa, or≥170 MPa, or ≥180 MPa, or ≥190 MPa, or ≥200 MPa. In another embodimentof the disclosure, a 1 mil film will have a machine direction (MD)secant modulus at 1% strain of from 150 MPa to 280 MPa. In an embodimentof the disclosure, a 1 mil film will have a machine direction (MD)secant modulus at 1% strain of from 160 MPa to 260 MPa. In an embodimentof the disclosure, a 1 mil film will have a machine direction (MD)secant modulus at 1% strain of from 170 MPa to 250 MPa. In anotherembodiment of the disclosure, a 1 mil film will have a machine direction(MD) secant modulus at 1% strain of from 180 MPa to 240 MPa. In anotherembodiment of the disclosure, a 1 mil film will have a machine direction(MD) secant modulus at 1% strain of from 180 MPa to 230 MPa.

In an embodiment of the disclosure, a 1 mil film will have a transversedirection (TD) secant modulus at 1% strain of ≥190 MPa, or ≥200 MPa, or≥210 MPa, or ≥220 MPa, or ≥230 MPa. In an embodiment of the disclosure,a 1 mil film will have a transverse direction (TD) secant modulus at 1%strain of from 160 MPa to 300 MPa. In another embodiment of thedisclosure, a 1 mil film will have a transverse direction (TD) secantmodulus at 1% strain of from 160 MPa to 280 MPa. In another embodimentof the disclosure, a 1 mil film will have a transverse direction (TD)secant modulus at 1% strain of from 170 MPa to 290 MPa. In anotherembodiment of the disclosure, a 1 mil film will have a transversedirection (TD) secant modulus at 1% strain of from 180 MPa to 290 MPa.In another embodiment of the disclosure, a 1 mil film will have atransverse direction (TD) secant modulus at 1% strain of from 190 MPa to280 MPa. In another embodiment of the disclosure, a 1 mil film will havea transverse direction (TD) secant modulus at 1% strain of from 190 MPato 270 MPa.

In embodiments of the disclosure, a 1 mil film will have a machinedirection (MD) tensile strength at break of >40 MPa, or >45 MPa, or >50MPa. In an embodiment of the disclosure, a 1 mil film will have amachine direction tensile strength at break of from 30 MPa to 70 MPa. Inan embodiment of the disclosure, a 1 mil film will have a machinedirection (MD) tensile strength at break of from 35 MPa to 70 MPa. Inanother embodiment of the disclosure, a 1 mil film will have a machinedirection (MD) tensile strength at break of from 40 MPa to 70 MPa.

In embodiments of the disclosure, a film will have a machine direction(MD) tear strength of ≥160 g/mil, or ≤170 g/mil, or ≥180 g/mil, or ≥190g/mil, or ≥200 g/mil, or ≥210 g/mil, or ≥220 g/mil, or ≥230 g/mil, or≥240 g/mil, or ≥250 g/mil. In an embodiment of the disclosure, a filmwill have a machine direction (MD) tear strength of from 150 g/mil to320 g/mil. In an embodiment of the disclosure, a film will have amachine direction (MD) tear strength of from 160 g/mil to 320 g/mil. Inan embodiment of the disclosure, a film will have a machine direction(MD) tear strength of from 160 g/mil to 310 g/mil. In an embodiment ofthe disclosure, a film will have a machine direction (MD) tear strengthof from 170 g/mil to 300 g/mil.

In embodiments of the disclosure, a 1 mil film will have a slow punctureresistance value of ≥45 J/mm, or ≥50 J/mm, or ≥55 J/mm. In embodimentsof the disclosure, a 1 mil film will have a slow puncture value of from40 J/mm to 90 J/mm, or from 50 J/mm to 90 J/mm, or from 50 J/mm to 80J/mm.

In embodiments of the disclosure, a 1 mil film will have a haze of ≤25%,or ≤23%, ≤20%, or ≤15%. In embodiments of the disclosure, a 1 mil filmwill have a haze of from 7% to 25%, or from 8% to 23%.

In embodiments of the disclosure, a 2 mil film will have a sealinitiation temperature (SIT) of ≤100° C., or ≤95° C., or ≤90° C., or≤85° C. In an embodiment of the disclosure, a 2 mil film will have aseal initiation temperature (SIT) of between 65° C. and 100° C. In anembodiment of the disclosure, a 2 mil film will have a seal initiationtemperature (SIT) of between 75° C. and 100° C. In an embodiment of thedisclosure, a 2 mil film will have a seal initiation temperature (SIT)of between 75° C. and 95° C. In an embodiment of the disclosure, a 2 milfilm will have a seal initiation temperature (SIT) of between 80° C. and95° C.

In an embodiment of the disclosure, a 1 mil film will have an oxygentransmission rate (OTR) of ≥600 cm³ per 100 inch². In an embodiment ofthe disclosure, a 1 mil film will have an oxygen transmission rate (OTR)of ≥650 cm³ per 100 inch². In an embodiment of the disclosure, a 1 milfilm will have an oxygen transmission rate (OTR) of ≥700 cm³ per 100inch². In an embodiment of the disclosure, a 1 mil film will have anoxygen transmission rate (OTR) of ≥740 cm³ per 100 inch². In anembodiment of the disclosure, a 1 mil film will have an oxygentransmission rate (OTR) of ≥800 cm³ per 100 inch². In an embodiment ofthe disclosure, a 1 mil film will have an oxygen transmission rate (OTR)of from 600 to 900 cm³ per 100 inch². In an embodiment of thedisclosure, a 1 mil film will have an oxygen transmission rate (OTR) offrom 650 to 900 cm³ per 100 inch². In an embodiment of the disclosure, a1 mil film will have an oxygen transmission rate (OTR) of from 700 to900 cm³ per 100 inch².

In an embodiment of the disclosure, a 2 mil film will have an area ofhot tack window (AHTW) of ≥160 Newtons·° C. In an embodiment of thedisclosure, a 2 mil film will have an area of hot tack window (AHTW) of≥170 Newtons·° C. In an embodiment of the disclosure, a 2 mil film willhave an area of hot tack window (AHTW) of ≥180 Newtons·° C. In anembodiment of the disclosure, a 2 mil film will have an area of hot tackwindow (AHTW) of from 160 to 260 Newtons·° C. In an embodiment of thedisclosure, a 2 mil film will have an area of hot tack window (AHTW) offrom 160 to 240 Newtons·° C. In an embodiment of the disclosure, a 2 milfilm will have an area of hot tack window (AHTW) of from 160 to 230Newtons·° C. In an embodiment of the disclosure, a 2 mil film will havean area of hot tack window (AHTW) of from 170 to 220 Newtons·° C. In anembodiment of the disclosure, a 2 mil film will have an area of hot tackwindow (AHTW) of from 170 to 200 Newtons·° C.

Some embodiments of the present disclosure provide films withimprovements in machine direction (MD) modulus (1% and/or 2%) and sealinitiation temperature relative to films formed from comparativepolyethylene. Hence, in an embodiment of the disclosure, a film layerhaving a thickness of from 0.5 to 10 mil, has a machine direction (MD)1% secant modulus of ≥180 MPa when measured at a film thickness of about1 mil and a seal initiation temperature (SIT) of <100° C. when measuredat a film thickness of about 2 mil. In another embodiment of thedisclosure, a film layer having a thickness of from 0.5 to 10 mil, has amachine direction (MD) 1% secant modulus of ≥190 MPa when measured at afilm thickness of about 1 mil and a seal initiation temperature (SIT) of≤95° C. when measured at a film thickness of about 2 mil. In anotherembodiment of the disclosure, a film layer having a thickness of from0.5 to 10 mil, has a machine direction (MD) 1% secant modulus of ≥200MPa when measured at a film thickness of about 1 mil and a sealinitiation temperature (SIT) of ≤95° C. when measured at a filmthickness of about 2 mil.

Some embodiments of the present disclosure provide films withimprovements in machine direction (MD) modulus (1% and/or 2%) and oxygentransmission rates (OTRs) relative to films formed from comparativepolyethylene. Hence, in an embodiment of the disclosure, a film layerhaving a thickness of from 0.5 to 10 mil, has a machine direction (MD)1% secant modulus of ≥190 MPa when measured at a film thickness of about1 mil and an oxygen transmission rate (OTR) of ≥650 cm³ per 100 inch²when measured at a film thickness of about 1 mil.

In an embodiment of the disclosure, the films manufactured using thepolyethylene compositions will have good hot tack performance. Good hottack performance is generally associated with good film performance inbag or pouch packaging lines, such as vertical-form-fill-seal (VFFS)applications lines. Without wishing to be bound by theory, in the hottack profile (seal temperature vs. force), good hot tack performance isindicated by an early (or low) hot tack initiation temperature, then arelatively high force over a wide range of seal temperatures.

Some embodiments of the present disclosure provide films withimprovements in machine direction (MD) modulus (1% and/or 2%) and areaof hot tack window (AHTW) relative to films formed from comparativepolyethylene. Hence, in an embodiment of the disclosure, a film layerhaving a thickness of from 0.5 to 10 mil, has a machine direction (MD)1% secant modulus of ≤190 MPa when measured at a film thickness of about1 mil and an area of hot tack window (AHTW) of ≥160 Newtons·° C. whenmeasured at a film thickness of about 2 mil.

Some embodiments of the present disclosure provide films withimprovements in machine direction (MD) modulus (1% and/or 2%), oxygentransmission rates, seal initiation temperature and area of hot tackwindow (AHTW) relative to films formed from comparative polyethylene.Hence, in an embodiment of the disclosure, a film layer having athickness of from 0.5 to 10 mil, has a has a machine direction (MD) 1%secant modulus of ≥190 MPa when measured at a film thickness of about 1mil, an oxygen transmission rate (OTR) of ≤650 cm³ per 100 inch² whenmeasured at a film thickness of about 1 mil, a seal initiationtemperature (SIT) of ≤100° C. when measured at a film thickness of about2 mil, and an area of hot tack window (AHTW) of ≤160 Newtons·° C. whenmeasured at a film thickness of about 2 mil.

In an embodiment of the disclosure, film satisfies the followingrelationship: area of hot tack window (AHTW)>−2.0981 (machine direction(MD) 1% secant modulus)+564.28; where the AHTW is measured at a filmthickness of about 2 mil, and the machine direction (MD) 1% secantmodulus is measured at a film thickness of about 1 mil.

In an embodiment of the disclosure, film satisfies the followingrelationship: oxygen transmission rate (OTR)>−5.4297 (machine direction(MD) 1% secant modulus)+1767.8; where the OTR is measured at a filmthickness of about 1 mil, and the machine direction (MD) 1% secantmodulus is measured at a film thickness of about 1 mil.

In an embodiment of the disclosure, film satisfies the followingrelationship: seal initiation temperature (SIT)<0.366 (machine direction(MD) 1% secant modulus)+22.509; where the SIT is measured at a filmthickness of about 2 mil, and the machine direction (MD) 1% secantmodulus is measured at a film thickness of about 1 mil.

In an embodiment of the disclosure, film satisfies each of the followingrelationships: i) area of hot tack window (AHTW)>−2.0981 (machinedirection (MD) 1% secant modulus)+564.28, where the AHTW is measured ata film thickness of about 2 mil, and the machine direction (MD) 1%secant modulus is measured at a film thickness of about 1 mil; ii)oxygen transmission rate (OTR)>−5.4297 (machine direction (MD) 1% secantmodulus)+1767.8, where the OTR is measured at a film thickness of about1 mil, and the machine direction (MD) 1% secant modulus is measured at afilm thickness of about 1 mil; and iii) seal initiation temperature(SIT)<0.366 (machine direction (MD) 1% secant modulus)+22.509, where theSIT is measured at a film thickness of about 2 mil, and the machinedirection (MD) 1% secant modulus is measured at a film thickness ofabout 1 mil.

In an embodiment of the disclosure, a film layer having a thickness offrom 0.5 to 10 mil, satisfies at least one of the followingrelationships: i) area of hot tack window (AHTW) −2.0981 (machinedirection (MD) 1% secant modulus)+564.28, where the AHTW is measured ata film thickness of about 2 mil, and the machine direction (MD) 1%secant modulus is measured at a film thickness of about 1 mil; ii)oxygen transmission rate (OTR)>−5.4297 (machine direction (MD) 1% secantmodulus)+1767.8, where the OTR is measured at a film thickness of about1 mil, and the machine direction (MD) 1% secant modulus is measured at afilm thickness of about 1 mil; and iii) seal initiation temperature(SIT)<0.366 (machine direction (MD) 1% secant modulus)+22.509, where theSIT is measured at a film thickness of about 2 mil, and the machinedirection (MD) 1% secant modulus is measured at a film thickness ofabout 1 mil.

In an embodiment of the disclosure, a film layer having a thickness offrom 0.5 to 10 mil, satisfies each of the following relationships: i)area of hot tack window (AHTW)>−2.0981 (machine direction (MD) 1% secantmodulus)+564.28, where the AHTW is measured at a film thickness of about2 mil, and the machine direction (MD) 1% secant modulus is measured at afilm thickness of about 1 mil; ii) oxygen transmission rate(OTR)>−5.4297 (machine direction (MD) 1% secant modulus)+1767.8, wherethe OTR is measured at a film thickness of about 1 mil, and the machinedirection (MD) 1% secant modulus is measured at a film thickness ofabout 1 mil; and iii) seal initiation temperature (SIT)<0.366 (machinedirection (MD) 1% secant modulus)+22.509, where the SIT is measured at afilm thickness of about 2 mil, and the machine direction (MD) 1% secantmodulus is measured at a film thickness of about 1 mil.

The films used in the manufactured articles described in this sectionmay optionally include, depending on its intended use, additives andadjuvants. Non-limiting examples of additives and adjuvants include,anti-blocking agents, antioxidants, heat stabilizers, slip agents,processing aids, anti-static additives, colorants, dyes, fillermaterials, light stabilizers, light absorbers, lubricants, pigments,plasticizers, nucleating agents and combinations thereof.

The following examples are presented for the purpose of illustratingselected embodiments of this disclosure; it being understood, that theexamples presented do not limit the claims presented.

EXAMPLES Test Methods

Prior to testing, each specimen was conditioned for at least 24 hours at23±2° C. and 50±10% relative humidity and subsequent testing wasconducted at 23±2° C. and 50±10% relative humidity. Herein, the term“ASTM conditions” refers to a laboratory that is maintained at 23±+2Cand 50±10% relative humidity; and specimens to be tested wereconditioned for at least 24 hours in this laboratory prior to testing.ASTM refers to the American Society for Testing and Materials.

Density was determined using ASTM D792-13 (Nov. 1, 2013).

Melt index was determined using ASTM D1238 (Aug. 1, 2013). Melt indexes,I₂, I₆, I₁₀ and I₂₁ were measured at 190° C., using weights of 2.16 kg,6.48 kg, 10 kg and a 21.6 kg respectively. Herein, the term “stressexponent” or its acronym “S.Ex.”, is defined by the followingrelationship: S.Ex.=log (I₆/I₂)/log(6480/2160); wherein I₆ and I₂ arethe melt flow rates measured at 190° C. using 6.48 kg and 2.16 kg loads,respectively.

M_(n), M_(w), and M_(z) (g/mol) were determined by high temperature GelPermeation Chromatography (GPC) with differential refractive index (DRI)detection using universal calibration (e.g. ASTM-D6474-99). GPC data wasobtained using an instrument sold under the trade name “Waters 150c”,with 1,2,4-trichlorobenzene as the mobile phase at 140° C. The sampleswere prepared by dissolving the polymer in this solvent and were runwithout filtration. Molecular weights are expressed as polyethyleneequivalents with a relative standard deviation of 2.9% for the numberaverage molecular weight (“Mn”) and 5.0% for the weight averagemolecular weight (“Mw”). The molecular weight distribution (MWD) is theweight average molecular weight divided by the number average molecularweight, M_(W)/M_(n). The z-average molecular weight distribution isM_(z)/M_(n). Polymer sample solutions (1 to 2 mg/mL) were prepared byheating the polymer in 1,2,4-trichlorobenzene (TCB) and rotating on awheel for 4 hours at 150° C. in an oven. The antioxidant2,6-di-tert-butyl-4-methylphenol (BHT) was added to the mixture in orderto stabilize the polymer against oxidative degradation. The BHTconcentration was 250 ppm. Sample solutions were chromatographed at 140°C. on a PL 220 high-temperature chromatography unit equipped with fourShodex columns (HT803, HT804, HT805 and HT806) using TCB as the mobilephase with a flow rate of 1.0 mL/minute, with a differential refractiveindex (DRI) as the concentration detector. BHT was added to the mobilephase at a concentration of 250 ppm to protect the columns fromoxidative degradation. The sample injection volume was 200 mL. The rawdata were processed with Cirrus GPC software. The columns werecalibrated with narrow distribution polystyrene standards. Thepolystyrene molecular weights were converted to polyethylene molecularweights using the Mark-Houwink equation, as described in the ASTMstandard test method D6474.

The short chain branch frequency (e.g. the short chain branching perthousand backbone carbon atoms, or the SCB/1000C) of ethylene copolymersamples was determined by Fourier Transform Infrared Spectroscopy (FTIR)as per the ASTM D6645-01 method. A Thermo-Nicolet 750 Magna-IRSpectrophotometer equipped with OMNIC version 7.2a software was used forthe measurements. Unsaturations in the polyethylene composition werealso determined by Fourier Transform Infrared Spectroscopy (FTIR) as perASTM D3124-98.

High temperature GPC equipped with an online FTIR detector (GPC-FTIR)was used to measure the comonomer content as the function of molecularweight.

Crystallization Elution Fractionation (CEF): A polymer sample (20 to 25mg) was weighed into the sample vial and loaded onto the auto-sampler ofthe Polymer CEF unit. The vail was filled with 6 to 7 ml1,2,4-trichlorobenzene (TCB), heated to the desired dissolutiontemperature (e.g. 160° C.) with a shaking rate of level number 3 for 2hours. The solution (0.5 ml) was then loaded into the CEF columns (twoCEF columns purchased from Polymer Char and installed in series). Afterallowed to equilibrate at a given stabilization temperature (e.g. 115°C.) for 5 minutes, the polymer solution was allowed to crystallize witha temperature drop from the stabilization temperature to 30° C. Afterequilibrating at 30° C. for 10 minutes, the soluble fraction was elutedat 30° C. for 10 minutes, followed by the crystallized sample elutedwith TCB with a temperature ramp from 30° C. to 110° C. The CEF columnswere cleaned at the end of the run for 5 minutes at 150° C. The otherCEF run conditions were as follows: cooling rate 0.5° C./minute, flowrate in crystallization 0.02 mL/minute, heating rate 1.0° C./minute andflow rate in elution 2.0 mL/minute. The data were processed using Excelspreadsheet. The “CDBI₅₀” is defined as the weight percent of ethylenepolymer whose composition is within 50% of the median comonomercomposition (50% on each side of the median comonomer composition). The“CDBI₅₀” may be calculated from the composition distribution curve,determined by the CEF procedure described above, and the normalizedcumulative integral of the composition distribution curve, asillustrated in U.S. Pat. No. 5,376,439 or WO 93/03093.

The “Composition Distribution Branching Index” or “CDBI” mayalternatively by determined using a crystal-TREF unit commerciallyavailable form Polymer ChAR (Valencia, Spain). The acronym “TREF” refersto Temperature Rising Elution Fractionation. A sample of thepolyethylene composition (80 to 100 mg) was placed in the reactor of thePolymer ChAR crystal-TREF unit, the reactor was filled with 35 ml of1,2,4-trichlorobenzene (TCB), heated to 150° C. and held at thistemperature for 2 hours to dissolve the sample. An aliquot of the TCBsolution (1.5 mL) was then loaded into the Polymer ChAR TREF columnfilled with stainless steel beads and the column was equilibrated for 45minutes at 110° C. The polyethylene composition was then crystallizedfrom the TCB solution, in the TREF column, by slowly cooling the columnfrom 110° C. to 30° C. using a cooling rate of 0.09° C. per minute. TheTREF column was then equilibrated at 30° C. for 30 minutes. Thecrystallized polyethylene composition was then eluted from the TREFcolumn by passing pure TCB solvent through the column at a flow rate of0.75 mL/minute as the temperature of the column was slowly increasedfrom 30° C. to 120° C. using a heating rate of 0.25° C. per minute.Using Polymer ChAR software a TREF distribution curve was generated asthe polyethylene composition was eluted from the TREF column, i.e. aTREF distribution curve is a plot of the quantity (or intensity) ofpolyethylene composition eluting from the column as a function of TREFelution temperature. A CDBI₅₀ may be calculated from the TREFdistribution curve for each polyethylene composition analyzed. The“CDBI₅₀” is defined as the weight percent of ethylene polymer whosecomposition is within 50% of the median comonomer composition (50% oneach side of the median comonomer composition); it is calculated fromthe TREF composition distribution curve and the normalized cumulativeintegral of the TREF composition distribution curve. Those skilled inthe art will understand that a calibration curve is required to converta TREF elution temperature to comonomer content, i.e. the amount ofcomonomer in the polyethylene composition fraction that elutes at aspecific temperature. The generation of such calibration curves aredescribed in references such as, e.g. Wild, et al., J. Polym. Sci., PartB, Polym. Phys., Vol. 20 (3), pages 441-455: hereby fully incorporatedby reference. Note: The “CDBI₂₅” is defined as the weight percent ofpolyethylene composition whose composition is within 25% of the mediancomonomer composition (25% on each side of the median comonomercomposition).

Dynamic mechanical analyses were carried out with a rheometer, namelyRheometrics Dynamic Spectrometer (RDS-II) or Rheometrics SR5 or ATSStresstech, on compression molded samples under nitrogen atmosphere at190° C., using 25 mm diameter cone and plate geometry. The oscillatoryshear experiments were done within the linear viscoelastic range ofstrain (10% strain) at frequencies from 0.05 to 100 rad/s. The values ofstorage modulus (G′), loss modulus (G″), complex modulus (G*) andcomplex viscosity (η*) were obtained as a function of frequency. Thesame rheological data can also be obtained by using a 25 mm diameterparallel plate geometry at 190° C. under nitrogen atmosphere. The Zeroshear viscosity is estimated using the Ellis model, i.e.η(ω)=η₀/(1+τ/τ_(1/2) ^(α-1), where η₀ is the zero shear viscosity.τ_(1/2) is the value of the shear stress at which η=η₀/2 and a is one ofthe adjustable parameters. The Cox-Merz rule is assumed to be applicablein the present disclosure.

The DRI, is the “dow rheology index”, and is defined by the equation:DRI=[365000(τ₀/η₀)−1]/10; wherein τ₀ is the characteristic relaxationtime of the polyethylene and η₀ is the zero shear viscosity of thematerial. The DRI is calculated by least squares fit of the rheologicalcurve (dynamic complex viscosity versus applied frequency e.g. 0.01-100rads/s) as described in U.S. Pat. No. 6,114,486 with the followinggeneralized Cross equation, i.e. η(ω)=η₀/[1+(ωτ₀)_(n)]; wherein n is thepower law index of the material, η(ω) and w are the measured complexviscosity and applied frequency data respectively. When determining theDRI, the zero shear viscosity, η₀ used was estimated with the Ellismodel, rather than the Cross model.

The crossover frequency is the frequency at which storage modulus (G′)and loss modulus (G″) curves cross with each other, while G′@G″=500 Pais the storage modulus at which the loss modulus (G″) is at 500 Pa.

Primary melting peak (° C.), melting peak temperatures (° C.), heat offusion (J/g) and crystallinity (%) was determined using differentialscanning calorimetry (DSC) as follows: the instrument was firstcalibrated with indium; after the calibration, a polymer specimen isequilibrated at 0° C. and then the temperature was increased to 200° C.at a heating rate of 10° C./min; the melt was then kept isothermally at200° C. for five minutes; the melt was then cooled to 0° C. at a coolingrate of 10° C./min and kept at 0° C. for five minutes; the specimen wasthen heated to 200° C. at a heating rate of 10° C./min. The DSC Tm, heatof fusion and crystallinity are reported from the 2^(nd) heating cycle.

Film dart impact strength was determined using ASTM D1709-09 Method A(May 1, 2009). In this disclosure the dart impact test employed a 1.5inch (38 mm) diameter hemispherical headed dart.

The film “ASTM puncture” is the energy (J/mm) required to break the filmwas determined using ASTM D5748-95 (originally adopted in 1995,reapproved in 2012). The puncture test is performed on a mechanicaltester, in which the puncture probe is attached to the load cell whichis mounted on a moving crosshead. The film is clamped into a clampingmechanism which has a 4 inch (102 mm) diameter opening. The clampingmechanism is attached to a fixed plate. The cross head speed is set at10 in/min (255 mm/min). The maximum force and energy to puncture thefilm are recorded.

The “slow puncture” or “lubricated puncture” test was performed asfollows: the energy (J/mm) to puncture a film sample was determinedusing a 0.75-inch (1.9-cm) diameter pear-shaped fluorocarbon coatedprobe travelling at 10-inch per minute (25.4-cm/minute). ASTM conditionswere employed. Prior to testing the specimens, the probe head wasmanually lubricated with Muko Lubricating Jelly to reduce friction. MukoLubricating Jelly is a water-soluble personal lubricant available fromCardinal Health Inc., 1000 Tesma Way, Vaughan, ON L4K 5R₈ Canada. Theprobe was mounted in an Instron Model 5 SL Universal Testing Machine anda 1000-N load cell as used. Film samples (1.0 mil (25 μm) thick, 5.5inch (14 cm) wide and 6 inch (15 cm) long) were mounted in the Instronand punctured. The following film tensile properties were determinedusing ASTM D882-12 (Aug. 1, 2012): tensile break strength (MPa),elongation at break (%), tensile yield strength (MPa), tensileelongation at yield (%) and film toughness or total energy to break(ft·lb/in³). Tensile properties were measured in the both the machinedirection (MD) and the transverse direction (TD) of the blown films.

The secant modulus is a measure of film stiffness. The secant modulus isthe slope of a line drawn between two points on the stress-strain curve,i.e. the secant line. The first point on the stress-strain curve is theorigin, i.e. the point that corresponds to the origin (the point of zeropercent strain and zero stress), and; the second point on thestress-strain curve is the point that corresponds to a strain of 1%;given these two points the 1% secant modulus is calculated and isexpressed in terms of force per unit area (MPa). The 2% secant modulusis calculated similarly. This method is used to calculated film modulusbecause the stress-strain relationship of polyethylene does not followHook's law; i.e. the stress-strain behavior of polyethylene isnon-linear due to its viscoelastic nature. Secant moduli were measuredusing a conventional Instron tensile tester equipped with a 200 lbf loadcell. Strips of monolayer film samples were cut for testing withfollowing dimensions: 14 inch long, 1 inch wide and 1 mil thick;ensuring that there were no nicks or cuts on the edges of the samples.Film samples were cut in both the machine direction (MD) and thetransverse direction (TD) and tested. ASTM conditions were used tocondition the samples. The thickness of each film was accuratelymeasured with a hand-held micrometer and entered along with the samplename into the Instron software. Samples were loaded in the Instron witha grip separation of 10 inch and pulled at a rate of 1 inch/mingenerating the strain-strain curve. The 1% and 2% secant modulus werecalculated using the Instron software.

The oxygen transmission rate (OTR) of the blown film was tested using anOxtran 2/20 instrument manufactured by MOCON Inc, Minneapolis, Minn.,USA. The instrument has two test cells (A and B) and each film samplewas analyzed in duplicate. The OTR result reported is the average of theresults from these two test cells (A and B). The test is carried out ata temperature of 23° C. and at a relative humidity of 0%. The filmsample area used for testing was 100 cm². The carrier gas used was 2%hydrogen gas in a balance of nitrogen gas and the test gas is ultra highpurity oxygen. The blown films which were tested each had a filmthickness of 1 mil.

Puncture-propagation tear resistance of blown film was determined usingASTM D2582-09 (May 1, 2009). This test measures the resistance of ablown film to snagging, or more precisely, to dynamic puncture andpropagation of that puncture resulting in a tear. Puncture-propagationtear resistance was measured in the machine direction (MD) and thetransverse direction (TD) of the blown films.

Film tear performance was determined by ASTM D1922-09 (May 1, 2009); anequivalent term for tear is “Elmendorf tear”. Film tear was measured inboth the machine direction (MD) and the transverse direction (TD) of theblown films.

Film optical properties were measured as follows: Haze, ASTM D1003-13(Nov. 15, 2013), and; Gloss ASTM D2457-13 (Apr. 1, 2013).

In this disclosure, the “Hot Tack Test” was performed as follows, usingASTM conditions. Hot tack data was generated using a J&B Hot Tack Testerwhich is commercially available from Jbi Hot Tack, Geloeslaan 30, B-3630Maamechelen, Belgium. In the hot tack test, the strength of a polyolefinto polyolefin seal is measured immediately after heat sealing two filmsamples together (the two film samples were cut from the same roll of2.0 mil (51-μm) thick film), i.e. when the polyolefin macromoleculesthat comprise the film are in a semi-molten state. This test simulatesthe heat sealing of polyethylene films on high speed automatic packagingmachines, e.g., vertical or horizontal form, fill and seal equipment.The following parameters were used in the J&B Hot Tack Test: filmspecimen width, 1 inch (25.4 mm); film sealing time, 0.5 second; filmsealing pressure, 0.27 N/mm²; delay time, 0.5 second; film peel speed,7.9 in/second (200 mm/second); testing temperature range, 131° F. to293° F. (55° C. to 145° C.); temperature increments, 9° F. (5° C.); andfive film samples were tested at each temperature increment to calculateaverage values at each temperature. In this way, a hot tack profile ofpulling force vs sealing temperature is generated. The following datacan be calculated from this hot tack profile: the “Tack Onset @ 1.0 N (°C.)”, is the temperature at which a hot tack force of 1N was observed(an average of five film samples); the “Max Hot tack Strength (N)”, isthe maximum hot tack force observed (an average of five film samples)over the testing temperature range; the “Temperature—Max. Hot tack (°C.)”, is the temperature at which the maximum hot tack force wasobserved. Finally, the area of the hot-tack (strength) window (the “areaof hot tack window” or the “AHTW”) is an estimate of the area under thishot tack profile from the hot-tack on-set temperature to the temperatureimmediately prior to the melting of the specimen. The latter temperatureprior to the melting of the specimen is typically at 130° C., but notnecessarily at 130° C. Piece-wise regressions (linear or polynomial)were performed for different segments of the hot tack profile to obtainthe mathematical relationships between seal temperature and pullingforce. The partial area of each temperature-force segment was thencalculated. The total area (AHTW) is the summation of each partial areaof each segment of the hot tack profile within the specified range(i.e., from the hot-tack on-set temperature to the temperatureimmediately prior to the melting of the specimen).

In this disclosure, the “Heat Seal Strength Test” (also known as “thecold seal test”) was performed as follows. ASTM conditions wereemployed. Heat seal data was generated using a conventional InstronTensile Tester. In this test, two film samples are sealed over a rangeof temperatures (the two film samples were cut from the same roll of 2.0mil (51-μm) thick film). The following parameters were used in the HeatSeal Strength (or cold seal) Test: film specimen width, 1 inch (25.4mm); film sealing time, 0.5 second; film sealing pressure, 40 psi (0.28N/mm²); temperature range, 212° F. to 302° F. (100° C. to 150° C.) andtemperature increment, 9° F. (5° C.). After aging for at least 24 hoursat ASTM conditions, seal strength was determined using the followingtensile parameters: pull (crosshead) speed, 12 inch/min (2.54 cm/min);direction of pull, 90° to seal, and; 5 samples of film were tested ateach temperature increment. The Seal Initiation Temperature, hereafterS.I.T., is defined as the temperature required to form a commerciallyviable seal; a commercially viable seal has a seal strength of 2.0 lb.per inch of seal (8.8 N per 25.4 mm of seal).

The hexane extractable content of a polymer sample was determinedaccording to the Code of Federal Registration 21 CFR § 177.1520 Para (c)3.1 and 3.2; wherein the quantity of hexane extractable material in afilm is determined gravimetrically. Elaborating, 2.5 grams of 3.5 mil(89 μm) monolayer film was placed in a stainless steel basket, the filmand basket were weighed (ω^(i)), while in the basket the film was:extracted with n-hexane at 49.5° C. for two hours; dried at 80° C. in avacuum oven for 2 hours; cooled in a desiccator for 30 minutes, and;weighed (ω^(f)). The percent loss in weight is the percent hexaneextractable (w^(C6)): w^(C6)=100×(w^(i)−w^(f))/w^(l).

Polyethylene Compositions

A polyethylene composition comprising a first, second and thirdpolyethylene was made by melt blending polyethylene composition A withpolyethylene B.

Polyethylene composition A was made using two different single sitecatalysts in a dual parallel reactor solution polymerization process. Asa result, polyethylene composition A comprised a first polyethylene madewith first single site catalyst (a metallocene) and a secondpolyethylene made with a second single site catalyst (a phosphiniminecatalyst). A parallel mode solution phase polymerization reactor processhas been described in U.S. patent application Ser. No. 15/491,264(co-pending with the present application). Basically, in parallel modethe exit streams exiting each of a first reactor (R1) and a secondreactor (R2) are combined downstream of each reactor and the polymerproduct is obtained after devolatilization.

The following examples illustrate the continuous solutioncopolymerization of ethylene and 1-octene at medium pressure in a dualreactor system connected in parallel. The first and second reactorpressure was about 16,000 kPa (about 2.3×10³ psi). The first reactor wasoperated at a lower temperature than the second reactor. The firstreactor had a volume of 12 liters and the second reactor had a volume of24 liters. Both reactors were agitated to ensure good mixing of thereactor contents. The process was continuous in all feed streams (i.e.solvents, which were methyl pentane and xylene; monomers and catalystand cocatalyst components) and in the removal of product. Monomer(ethylene) and comonomer (1-octene) were purified prior to addition tothe reactor using conventional feed preparation systems (such as contactwith various absorption media to remove impurities such as water, oxygenand polar contaminants). The reactor feeds were pumped to the reactorsat the ratios shown in Table 1. Average residence times for the reactorsare calculated by dividing average flow rates by reactor volume. Theresidence time in each reactor for all of the inventive experiments wasless than 10 minutes and the reactors were well mixed. The catalystdeactivator used was octanoic acid (caprylic acid), commerciallyavailable from P&G Chemicals, Cincinnati, Ohio, U.S.A.

The following single site catalyst (SSC) components were used to preparethe first polyethylene in a first reactor (R₁) configured in parallel toa second reactor (R₂):diphenylmethylene(cyclopentadienyl)(2,7-di-t-butylfuorenyl)hafniumdimethide [(2,7-tBu₂Flu)Ph₂C(Cp)HfMe₂]; methylaluminoxane (MMAO-07);trityl tetrakis(pentafluoro-phenyl)borate (trityl borate), and2,6-di-tert-butyl-4-ethylphenol (BHEB). Methylaluminoxane (MMAO-07) and2,6-di-tert-butyl-4-ethylphenol are premixed in-line and then combinedwith diphenylmethylene(cyclopentadienyl)(2,7-di-t-butylfuorenyl)hafniumdimethide and trityl tetrakis(pentafluoro-phenyl)borate just beforeentering the polymerization reactor (R1).

The following single site catalyst (SSC) components were used to preparethe first polyethylene in a second reactor (R₂) configured in parallelto a first reactor (R₁): cyclopentadienyl tri(tertiarybutyl)phosphinimine titanium dichloride [Cp((t-Bu)₃PN)TiCl₂];methylaluminoxane (MMAO-07); trityl tetrakis(pentafluoro-phenyl)borate(trityl borate), and 2,6-di-tert-butyl-4-ethylphenol (BHEB).Methylaluminoxane (MMAO-07) and 2,6-di-tert-butyl-4-ethylphenol arepremixed in-line and then combined with cyclopentadienyltri(tertiarybutyl)phosphinimine titanium dichloride [Cp((t-Bu)₃PN)TiCl₂]and trityl tetrakis(pentafluoro-phenyl)borate just before entering thepolymerization reactor (R₂).

Polyethylene C, on the other hand is made in a single solutionpolymerization reactor using a Ziegler-Natta catalyst as describedbelow; however, in this example the in-line formed Ziegler-Nattacatalyst was fed only to a first reactor (R₁) to prepare polyethylene Cin a single reactor. For the sake of clarity, polyethylene C becomes thethird polyethylene within the final polyethylene composition. Thefollowing Ziegler-Natta (ZN) catalyst components were used to preparethe third polyethylene: butyl ethyl magnesium; tertiary butyl chloride;titanium tetrachloride; diethyl aluminum ethoxide; and triethylaluminum. Methylpentane was used as the catalyst component solvent andthe in-line Ziegler-Natta catalyst formulation was prepared using thefollowing steps. In step one, a solution of triethylaluminum and butylethyl magnesium (Mg:Al=20, mol:mol) was combined with a solution oftertiary butyl chloride and allowed to react for about 30 seconds toproduce a MgCl₂ support. In step two, a solution of titaniumtetrachloride was added to the mixture formed in step one and allowed toreact for about 14 seconds prior to injection into reactor (R₁). Thein-line Ziegler-Natta catalyst was activated in the reactor by injectinga solution of diethyl aluminum ethoxide into R₁. The quantity oftitanium tetrachloride added to the reactor is shown in Table 1. Theefficiency of the in-line Ziegler-Natta catalyst formulation wasoptimized by adjusting the mole ratios of the catalyst components.

Table 1, shows the reactor conditions used to make polyethylenecomposition A, as well as polyethylene B. The properties of polyethylenecomposition A, as well as polyethylene B are shown in Table 2.

TABLE 1 Reactor Operating Conditions Blending Component PE Composition ASSC in R1 and SSC PE B in R2 (dual reactor ZN in R1 (single Descriptionin parallel mode) reactor) Reactor 1 (R1) metallocene ZN TSR (kg/hr) 300375 Ethylene concentration 7.9 9.3 (wt %) 1-Octene/ethylene in 0.82 0.65fresh feed (g/g) Primary feed 35.0 35.0 temperature (° C.) MeanTemperature (° C.) 130.2 150.8 Ethylene conversion 80.1 91.3 HydrogenFeed (ppm) 0.49 3.75 Catalyst (ppm) to R1 0.84 4.7 SSC - Al/Hf (mol/mol)31 N/A SSC - BHEB/Al 0.4 N/A (mol/mol) SSC - B/Hf (mol/mol) 1.22 N/AZN - N/A 2.1 tertbutylchloride/Mg (mol/mol) ZN - Mg/Ti (mol/mol) N/A 7.0ZN - diethyl aluminum N/A 1.35 ethoxide/Ti (mol/mol) Reactor 2 (R2)phosphinimine TSR (kg/hr) 300 N/A Ethylene concentration 13.4 N/A (wt %)1-Octene/ethylene in 0.0 N/A fresh feed (g/g) Primary feed 35.3 N/Atemperature (° C.) Mean Temperature (° C.) 190.9 N/A Ethylene conversion90.0 N/A Hydrogen Feed (ppm) 5.31 N/A Catalyst (ppm) to R2 0.24 N/ASSC - Al/Ti (mol/mol) 65 N/A SSC - BHEB/Al 0.3 N/A (mol/mol) SSC - B/Ti(mol/mol) 1.5 N/A

TABLE 2 Blend Component Properties Blending Component PE Composition ASSC in R1 and SSC in R2 (dual PE B reactor in parallel ZN in R1Description mode) (single reactor) Catalysts SSC/SSC ZN PS Sample No./PS-125595 PS-125534 NOVA Lot No. Density (g/cm³) 0.9152 0.9164 MeltIndex I₂ (g/10 min) 1.49 0.33 Melt Index I₆ (g/10 min) 6.95 1.36 MeltIndex I₁₀ (g/10 min) 13.4 2.46 Melt Index I₂₁ (g/10 min) 52.2 8.74 MeltFlow Ratio 35 26.50 (I₂₁/I₂) Stress Exponent 1.40 1.28 Melt Flow Ratio9.12 7.70 (I₁₀/I₂) Branch Frequency - FTIR Branch Freq/1000 C. 21.5 15.7Comonomer 1-octene 1-octene Comonomer 4.30 3.10 Content (mole %)Comonomer 15.2 11.5 Content (weight %) Internal 0.013 0.005 Unsat/100 C.Side Chain 0.002 0.002 Unsat/100 C. Terminal 0.006 0.025 Unsat/100 C.GPC - Conventional M_(n) 49016 34317 M_(w) 105906 135987 M_(z) 215295338832 Polydispersity 2.16 3.96 Index (M_(w)/M_(n))

The properties of two different polyethylene compositions which wereobtained from melt blending polyethylene composition A with polyethyleneB at two different weight fractions is provided in Table 3 as InventiveExamples 1 and 2. The materials were melt blended using a Coperion ZSK26 co-rotating twin screw extruder with an L/D of 32:1. The extruder wasfitted with an underwater pelletizer and a Gala spin dryer. Thematerials were co-fed to the extruder using gravimetric feeders toachieve the desired ratios of polyethylene composition A to polyethyleneB. The blends were compounded using a screw speed of 200 rpm at anoutput rate of 15-20 kg/hour and at a melt temperature of 225-230° C.

Data for comparative polyethylene compositions, Comparative Examples 1-9is also included in Table 3. Comparative Example 1 is ELITE® 5400G, aresin commercially available from the Dow Chemical Company. ELITE 5400Ghas a density of about 0.916 g/cm³ and a melt index I₂ of about 1dg/min. Comparative Example 2 is SURPASS® FP117-C, a resin commerciallyavailable from the NOVA Chemicals Corporation. SURPASS FP117-C has adensity of 0.917 g/cm³ and a melt index I₂ of 1 dg/min. ComparativeExamples 3 and 4 are resins made according to U.S. Pat. Appl. Pub. No.2016/0108221. Comparative Example 3 is an ethylene/1-octene copolymer,has a density of about 0.917 g/cm³, a melt index I₂ of about 0.96dg/min, and is made in a multi reactor solution process in which a firstreactor and a second reactor are configured in series with one another.Comparative Example 4 is an ethylene/1-octene copolymer, has a densityof about 0.913 g/cm³, a melt index I₂ of about 0.85 dg/min, and is madein a multi reactor solution process in which a first reactor and asecond reactor are configured in series with one another. ComparativeExample 5 is SCLAIR® FP112-A, a resin commercially available from theNOVA Chemicals Corporation. SCLAIR FP112-A has a density of 0.912 g/cm³and a melt index I₂ of 0.9 dg/min. Comparative Example 6 is EXCEED®⁰1018CA, a resin commercially available from ExxonMobil. EXCEED 1018CAhas a density of about 0.918 g/cm³ and a melt index I₂ of about 0.94dg/min. Comparative Example 7 is MARLEX® D139, a resin commerciallyavailable from ChevronPhillips. MARLEX D139 has a density of about 0.918g/cm³ and a melt index I₂ of about 0.9 dg/min. Comparative Example 8 isSCLAIR® FP120-A, a resin commercially available the NOVA ChemicalsCorporation. FP120-A has a density of 0.920 g/cm³ and a melt index I₂ of1 dg/min. Comparative Example 9 is SCLAIR® FP026-F, a resin commerciallyavailable the NOVA Chemicals Corporation. FP026-F has a density of 0.926g/cm³ and a melt index I₂ of 0.75 dg/min.

TABLE 3 Polyethylene Composition Properties Example No. Invention 1 Inv.2 (70 wt % PE (40 wt % PE Composition A/ Composition A/ 30 wt % PE B) 60wt % PE B) Comp. 1 Comp. 2 Comp. 3 Comp. 4 Density (g/cm³) 0.9159 0.91620.9159 0.9166 0.9167 0.913 Melt Index I₂ 0.73 0.48 1 0.99 0.96 0.85(g/10 min) Melt Index I₆ 3.48 2.14 4.46 4 3.72 3.09 (g/10 min) MeltIndex I₁₀ 6.68 4.02 8.57 7.57 6.65 (g/10 min) Melt Index I₂₁ 26.4 15.531.3 29 24.4 (g/10 min) Melt Flow 36.3 32.5 31.4 29.4 25.4 21.5 Ratio(I₂₁/I₂) Stress 1.42 1.36 1.36 1.27 1.23 1.21 Exponent Melt Flow 9.528.72 8.61 7.67 7.24 6.78 Ratio (I₁₀/I₂) Rheological Properties ZeroShear 19940 23400 15600 8688 9433 11350 Viscosity - 190° C. (Pa-s)Crossover 80.53 50.76 110.98 73.56 81.27 98.88 Frequency - 190° C.(rad/s) DRI 1.78 0.78 2.41 0.26 0.23 0.22 G′@G″500 Pa = 133.18 82.9279.3 22.8 23.9 32 Branch Frequency - FTIR Branch 19.7 17.7 15.2 14.115.6 17.1 Freq/1000 C Comonomer 1-octene 1-octene 1-octene 1-octene1-octene 1-octene Comonomer 3.9 3.5 3 2.8 3.1 3.4 Content (mole %)Comonomer 14.1 12.8 11.2 10.4 11.4 12.7 Content (wt %) Internal 0.0090.007 0.003 0.019 0.009 0.007 Unsat/100 C Side Chain 0.006 0.005 0.0040.003 0.006 0.003 Unsat/100 C Terminal 0.012 0.02 0.029 0.006 0.0460.027 Unsat/100 C CEF Soluble 30.33 19.4 2.05 0.77 3.78 2.42 fraction(%), ≤30° C. DSC First Melting 128.100 113.600 101 109 105.7 100.0 Peak(° C.) Second 126 118 112 117.4 119.3 Melting Peak (° C.) Third Melting— 122 — 121.2 122.8 Peak (° C.) Heat of Fusion 127 126.3 119 123 123.9112.6 (J/g) Crystallinity 43.8 43.6 41.19 42.29 42.72 38.82 (%) GPC -Conventional M_(n) 45974 46076 36781 33939 33939 44573 M_(w) 119291123764 99802 102503 102503 114666 M_(z) 277605 284944 210866 234321234321 262824 Polydispersity 2.59 2.69 2.71 3.02 3.02 2.57 Index(M_(w)/M_(n)) Mz/Mw 2.33 2.30 2.11 2.29 2.29 2.29 Hexane 3.17 0.87 0.540.56 0.77 0.61 Extractables (%) - Plaque Example No. Comp. 5 Comp. 6Comp. 7 Comp. 8 Comp. 9 Density (g/cm³) 0.912 0.919 0.918 0.920 0.926Melt Index I₂ 0.9 0.94 0.89 1 0.75 (g/10 min) Melt Index I₆ 3.16 3.144.29 3.02 (g/10 min) Melt Index I₁₀ 5.16 5.22 — — (g/10 min) Melt IndexI₂₁ 14.8 15.2 29.8 20.1 (g/10 min) Melt Flow 31.4 15.8 17.2 29.8 27Ratio (I₂₁/I₂) Stress 1.34 1.11 1.15 1.32 1.31 Exponent Melt Flow 5.645.94 — — Ratio (I₀/I₂) Rheological Properties Zero Shear 12990 7731 919810783 14750 Viscosity - 190° C. (Pa-s) Crossover 83.76 159.80 149.38107.5 91.93 Frequency - 190° C. (rad/s) DRI 0.01 0.09 — — G′@G″500 Pa =45.7 8 34.1 41.9 47.7 Branch Frequency - FTIR Branch 19.2 13.4 13.1Freq/1000 C Comonomer 1-octene 1-hexene 1-hexene 1-octene 1-octeneComonomer 3.8 2.7 2.6 2.6 1.7 Content (mole %) Comonomer 13.8 9.9 9.79.7 6.3 Content (wt %) Internal 0.007 0.002 0.006 0.005 0.002 Unsat/100C Side Chain 0.007 0.004 0.005 0.006 0.004 Unsat/100 C Terminal 0.0450.01 0.007 0.052 0.048 Unsat/100 C CEF Soluble 7.13 0.57 0.57 2.85 1.14fraction (%), ≤30° C. DSC First Melting 102.0 109.52 106.26 108.93115.24 Peak (° C.) Second 117.9 118.08 116.62 119.52 121.5 Melting Peak(° C.) Third Melting 121.6 — — — Peak (° C.) Heat of Fusion 110.6 126.96125.56 132.95 144.24 (J/g) Crystallinity 38.14 43.78 43.29 45.84 49.74(%) GPC - Conventional M_(n) 33139 55850 55399 31575 35549 M_(w) 118358110641 106175 101954 112255 M_(z) 379353 186289 180670 302775 297745Polydispersity 3.57 1.98 1.92 3.40 3.16 Index (M_(w)/M_(n)) Mz/Mw 3.211.68 1.70 2.82 2.65 Hexane 1.40 0.26 0.37 0.44 0.22 Extractables (%) -Plaque

Details of the Inventive polyethylene composition components: the firstpolyethylene, the second polyethylene, and the third polyethylene, areprovided in Table 4. With the exception of the weight percentages, w1and w2 (which are found by adjusting the de-convoluted values, w1′ andw2′, as is further discussed below) the data in Table 4 includes themathematically de-convoluted component properties of polyethylenecomposition A (which comprised the first polyethylene which was madewith a single site metallocene catalyst and the second polyethylenewhich was made with a single site phosphinimine catalyst) as well as theexperimentally determined properties of polyethylene B (the thirdpolyethylene which was made with a Ziegler-Natta catalyst).

High temperature GPC equipped with an online FTIR detector (GPC-FTIR)was used to measure the comonomer content as a function of molecularweight. In order to de-convolute the polyethylene composition A (whichresults from use of a SSC in R1 and R2 in parallel mode polymerization)into components, the mathematical deconvolution model described in U.S.Pat. No. 8,022,143 was used. The mathematical deconvolution of the GPCand GPC-FTIR data, the molecular weight distribution of the firstpolyethylene (the SSC component made in R₁, considered one catalystsite) and the second polyethylene (the SSC component made in R₂,considered one catalyst site) was modeled using a single Schultz Florydistribution (where the Mw/Mn was assumed to be 2; the M_(n) was M_(w)/2and the Mz was 1.5×Mw) as described in U.S. Pat. No. 8,022,143. Toimprove the deconvolution accuracy and consistency, as a constraint, themelt index, I₂, of the modeled composition (i.e. the dual-reactorpolyethylene composition A) was set and the following relationship wassatisfied during the deconvolution:

Log₁₀(I ₂)=22.326528+0.003467*[Log₁₀(M _(n))]³−4.322582*Log₁₀(M_(w))-0.180061*[Log₁₀(Mz)]²+0.026478*[Log₁₀(Mz)]³

where the experimentally measured overall melt index (i.e. ofpolyethylene composition A), 12, was used on the left side of theequation. Hence, a total of two sites (one for each SSC) were used tode-convolute polyethylene composition A. The w(i) and M_(n)(i), i=1 to2, were obtained while M_(w)(i) and Mz(i) of each site were calculatedusing the above relationships using M_(n)(i) for each site. During thedeconvolution, the overall M_(n), M_(w) and M_(z) of polyethylenecomposition A was calculated with the following relationships:M_(n)=1/Sum(w_(i)/M_(n)(i)), M_(w)=Sum(w_(i)×M_(w)(i)),M_(z)=Sum(w_(i)×M₂(i)²), where i represents the i-th component and w_(i)represents the relative weight fraction of the i-th component in thecomposition from the above 2-site deconvolution. The GPC-FTIRchromatograph profile was subsequently deconvoluted using the w(i)results to obtain SCB(i), i=1 to 2.

The M_(n), M_(w), Mz and SCB/1000C of the first and second polyethylenesmade with a SSC in each of R₁ and R₂ were then calculated using theabove relationships, with the above data of M_(n)(i), M_(w)(i), Mz(i),SCB(i) for each catalyst site.

When the polymer made with the single site catalyst in R₂ was anethylene homopolymer, as is the case in the present examples, thenduring the deconvolution analysis the SCB/1000C for the modeled SSC sitewas set as zero. If however, the polymer made by the SSC was acopolymer, then the SCB value would be determined for the SSC site usingthe deconvolution model presented above.

In order to calculate the melt index, I₂ of each of the first and secondpolyethylenes in polyethylene composition A, the following melt index,I₂ model was used:

Log₁₀(melt index,I ₂)=22.326528+0.003467*[Log₁₀(M_(n))]³≤4.322582*Log₁₀(M _(w))−0.180061*[Log₁₀(M_(z))]²+0.026478*[Log₁₀(M _(z))]³

where the M_(n), M_(w) and M_(z) were the deconvoluted values of thefirst or second polyethylene components present in polyethylenecomposition A, as obtained from the results of the above GPCdeconvolution.

The density of the first polyethylene which was an ethylene copolymermade using a single site catalyst in R1 was calculated using thefollowing density model: density of the first polyethylene made with aSSC=0.979863-0.00594808*(FTIRSCB/1000C)^(0.65)−0.000383133*[Log₁₀(M_(n))]³−0.00000577986*(M_(w)/M_(n))³+0.00557395*(M_(Z)/M_(w))^(0.25)

where the M_(n), M_(w) and M_(z) were the deconvoluted values of thefirst polyethylene as obtained from the results of the above GPCdeconvolution and the SCB/1000C was obtained from the GPC-FTIRdeconvolution. The density of the second polyethylene which was anethylene homopolymer made with a single site catalyst in R₂ wasdetermined using the same equation used above for finding the density ofthe first polyethylene, but with the value for the short chain branchingset to zero to cancel out the corresponding term:

density of the second polyethylene made with aSSC=0.979863−0.000383133*[Log₁₀(M _(n))]³−0.00000577986*(M _(w) /M_(n))³+0.00557395*(M _(z) /M _(w))^(0.25).

The de-convolution provided the density (d1, and d2), melt index (I₂ ¹and I₂ ²), short chain branching (SCB1 with the SCB2 being set as zerofor an ethylene homopolymer) the weight average and number averagemolecular weights (Mw1, M_(n)1, M_(w)2 and M_(n)2), and the weightfraction (ω1′ and w2′) of the first and second polyethylenes Theresulting deconvoluted properties as well as the relative weightpercentages w1, w2 (which for the first and the second polyethylenes,respectively, are found by modifying the deconvoluted weight fractionsw1′ and w2′ to match the amount of polyethylene composition A in thefinal melt blended polyethylene composition, as determined by theblending rules discussed further below) are provided in Table 4.

The following basic blending rules were used to achieve the desiredpolyethylene compositions comprising a first, a second and a thirdpolyethylene:

w1=weight percentage of the first polyethylene in the final polyethylenecomposition;

-   -   w2=weight percentage of the second polyethylene in the final        polyethylene composition;    -   w3=weight percentage of the third polyethylene in the final        polyethylene composition;    -   w1*=weight percentage of polyethylene composition A in the melt        blend; w2*=weight percentage of polyethylene B in the melt        blend;    -   w1′=weight percentage of the first polyethylene in polyethylene        composition A (i.e. the w1′ determined from the mathematical        deconvolution of polyethylene composition A);    -   w2′=weight percentage of the second polyethylene in polyethylene        composition A (i.e. the w2′ determined from the mathematical        deconvolution of polyethylene composition A);    -   where,        -   w1+w2+w3=1;        -   w1*+w2*=1; and        -   w1′+w2′=1;    -   so that,        -   w1=w1*×w1′;        -   w2=w1*×w2′; and        -   w3=w2*.

TABLE 4 Polyethylene Composition Component Properties Example No.Inventive PE Inventive PE Composition 1 Composition 2 PolyethyleneComposition Density (g/cm³) 0.9159 0.9162 I₂ (dg/min) 0.73 0.48 StressExponent 1.42 1.36 MFR (I₂₁/I₂) 36.3 32.5 Mn 45974 46076 Mw 119291123764 Mz 277605 284944 Mw/Mn 2.59 2.69 Mz/Mw 2.33 2.30 The FirstPolyethylene Catalyst Type 1 Single Site Catalyst Single Site Catalyst(metallocene) (metallocene) weight fraction, w1 0.308 0.176 (note: w1′ =0.44 from (note: w1′ = 0.44 from deconvolution) deconvolution) Mn1 6575065750 Mw1 131500 131500 Mw1/Mn1 2 (Mw1/Mn1 < 2.3) 2 (Mw1/Mn1 < 2.3)short chain branches per 49 49 1000 carbons I₂ ¹ (g/10 min.) 0.3 0.3 d1(g/cm³) 0.8685 0.8685 The Second Polyethylene Catalyst Type 2 SingleSite Catalyst Single Site Catalyst (phosphinimine) (phosphinimine)weight fraction, w2 0.392 0.224 (note: w2′ = 0.56 from (note: w2′ = 0.56from deconvolution) deconvolution) Mn2 25450 25450 Mw2 50900 50900Mw2/Mn2 2 (Mw2/Mn2 < 2.3) 2 (Mw2/Mn2 < 2.3) short chain branches per 0 01000 carbons I₂ ² (g/10 min) 11.67 11.67 d2 (g/cm³) 0.9532 0.9532 TheThird Polyethylene Catalyst Type 3 Ziegler-Natta Catalyst Ziegler-NattaCatalyst weight fraction, w3 0.300 0.600 Mn3 34317 34317 Mw3 135987135987 Mw3/Mn3 3.96 (Mw3/Mn3 > 2.3) 3.96 (Mw3/Mn3 > 2.3) short chainbranches per 15.7 15.7 1000 carbons I₂ ³ (g/10 min) 0.33 0.33 d3 (g/cm³)0.9164 0.9164

With reference to FIG. 1, a person skilled in the art will recognizethat the inventive polyethylene compositions have a unimodal GPCprofile.

With reference to FIG. 2, a person skilled in the art will recognizethat the inventive polyethylene compositions have a partially reversecomonomer incorporation, where the comonomer incorporation first risesas molecular weight increases, and then falls as the molecular weightincreases still further.

With reference to FIG. 3, a person skilled in the art will recognizethat the inventive polyethylene compositions each have a melting peakwhich occurs at above 125° C. For Inventive Example 1 the DSC profile isunimodal. For Inventive Example 2, the DSC profile is bimodal.

The data in Table 3, clearly shows that in contrast to each of thecomparative resins, the inventive polyethylene compositions have asignificant amount of material eluting at lower temperature in acrystallization elution fractionation (CEF) analysis. Inventive Examples1 and 2, each have a soluble fraction in a crystallization elutionfractionation (CEF) analysis of greater than 10 weight percent(Inventive Example 1, is 30.3 weight percent; Inventive Example 2, is19.4 weight percent), while all of the Comparative Examples 1-9, have asoluble fraction in a crystallization elution fractionation (CEF)analysis (i.e. a fraction eluting at or below 30° C.) of less than 10weight percent.

Blown films were generated by using a 2.5-inch Gloucester blown filmline (L/D=24) with a die diameter of 4-inch. The die was coated withpolymer processing aid (PPA) by spiking the line with a highconcentration of PPA masterbatch to avoid melt fracture. The fixedconditions were die gap of 35 mils (0.0889 cm), frost line height ofabout 17 inches and output of 100 lbs/hr. Films were collected underdifferent orientation conditions. The monolayer 1-mil film was producedwith a blow up ratio (BUR) of 2.5 and the 1-mil films were used forobtaining the physical properties of the films. The monolayer 2-mil film(BUR=2.5) was used for obtaining the cold-seal and hot tack profiles.Data for film blown from the polyethylene compositions of the presentdisclosure is provided in Table 5, along with data for films made fromvarious comparative resins.

Comparative Example 1 is a film made from ELITE® 5400G, a resincommercially available from the Dow Chemical Company. ELITE 5400G has adensity of about 0.916 g/cm³ and a melt index I₂ of about 1 dg/min.Comparative Example 2 is a film made from SURPASS® FP117-C, a resincommercially available from the NOVA Chemicals Corporation. SURPASSFP117-C has a density of 0.917 g/cm³ and a melt index I₂ of 1 dg/min.Comparative Examples 3 and 4 are films made from resins made accordingto US Pat. Appl. Pub. No. 2016/0108221. Comparative Example 3 is a filmmade from an ethylene/1-octene copolymer which has a density of about0.917 g/cm³, a melt index I₂ of about 0.96 dg/min, and which was made ina multi reactor solution process in which a first reactor and a secondreactor are configured in series with one another. Comparative Example 4is a film made from an ethylene/1-octene copolymer which has a densityof about 0.913 g/cm³, a melt index I₂ of about 0.85 dg/min, and whichwas made in a multi reactor solution process in which a first reactorand a second reactor are configured in series with one another.Comparative Example 5 is a film made from SCLAIR® FP112-A, a resincommercially available from the NOVA Chemicals Corporation. SCLAIRFP112-A has a density of 0.912 g/cm³ and a melt index I₂ of 0.9 dg/min.Comparative Example 6 is a film made from EXCEED® 1018CA, a resincommercially available from ExxonMobil. EXCEED 1018CA has a density ofabout 0.918 g/cm³ and a melt index I₂ of about 0.94 dg/min. ComparativeExample 7 is a film made from MARLEX® D139, a resin commerciallyavailable from ChevronPhillips. MARLEX D139 has a density of about 0.918g/cm³ and a melt index I₂ of about 0.9 dg/min. Comparative Example 8 isa film made from SCLAIR® FP120-A, a resin commercially available theNOVA Chemicals Corporation. FP120-A has a density of 0.920 g/cm³ and amelt index I₂ of 1 dg/min. Comparative Example 9 is a film made fromSCLAIR® FP026-F, a resin commercially available the NOVA ChemicalsCorporation. FP026-F has a density of 0.926 g/cm³ and a melt index I₂ of0.75 dg/min. In Table 5, the Inventive Examples 1 and 2, are films madefrom the Inventive polyethylene compositions of Inventive Examples 1 and2.

TABLE 5 Film Properties Example No. Inventive PE Inventive PEComposition 1 Composition 2 Comparative 1 Comparative 2 Film PhysicalProperties Thickness Profile Ave 1 1 1.03 1.01 Film Toughness DartImpact (g/mil) 602 784 818 470 Slow Puncture - Lube/Tef 56 69 63 85(J/mm) ASTM Puncture (J/mm) 136 165 97 Film Tear Resistance Tear - MD(g/mil) 174 286 247 308 Tear - TD (g/mil) 505 598 485 516 Film Stiffness1% Sec Modulus - MD 204 216 165 129 (Mpa) 1% Sec Modulus - TD 248 239175 131.4 (Mpa) 2% Sec Modulus - MD 173 183 151 117 (Mpa) 2% SecModulus - TD 209 201 155 123.8 (Mpa) Film Tensile Strength Tensile BreakStr - MD 49.4 57.4 44 46.4 (Mpa) Tensile Break Str - TD 40.4 44.2 45.548 (Mpa) Elongation at Break - MD 583 513 486 534 (%) Elongation atBreak - TD 779 757 725 796 (%) Tensile Yield Str - MD 10.41 10.6 9.1 8.8(Mpa) Tensile Yield Str - TD 11.5 11.3 8.7 8.8 (Mpa) Tensile Elong atYield - 10 10 13 22 MD (%) Tensile Elong at Yield - 10 10 13 17 TD (%)Film Opticals Gloss at 45° 32 57 64 50 Haze (%) 19.6 9.7 7.8 12 ColdSeal Properties S.I.T. @ 8.8 N Seal 81.7 94.1 100.4 98.8 Strength (° C.)Max Force (N) 25.1 28 24.9 19.9 Temp. @ Max Force (° C.) 160 160 150 130Hot Tack Properties Tack Onset @ 1.0 N (° C.) - 63.5 70.5 92.5 100.5 2mil film Max Hottack Strength (N) - 3.28 4.3 5.4 4.1 2 mil filmTemperature - Max. 120 120 110 115 Hottack (° C.) - 2 mil film AHTW(Newtons · ° C.) 189.1 183.1 140 95.3 OTR (cm³ per 100 inch²) 847.4746.1 — 662.8 Example No. Comparative 3 Comparative 4 Comparative 5Comparative 6 Comparative 7 Film Physical Properties Thickness ProfileAve 1.04 1 1 1.01 1.03 Film Toughness Dart Impact (g/mil) 812 891 546827 688 Slow Puncture - Lube/Tef 98 80 77 (J/mm) ASTM Puncture (J/mm) 66151 84 Film Tear Resistance Tear - MD (g/mil) 293 231 376 241 186 Tear -TD (g/mil) 540 548 580 358 454 Film Stiffness 1% Sec Modulus - MD 150.4145 113 156.8 177.6 (Mpa) 1% Sec Modulus - TD 167.8 134 111 168.8 185(Mpa) 2% Sec Modulus - MD 141.4 149 136 150.2 166.4 (Mpa) 2% SecModulus - TD 149.2 136 127 161.4 170.2 (Mpa) Film Tensile StrengthTensile Break Str - MD 45.4 51.8 56.4 50.7 47.8 (Mpa) Tensile BreakStr - TD 44.6 50.6 53.5 61.1 47.8 (Mpa) Elongation at Break - MD 521 557479 566 505 (%) Elongation at Break - TD 747 751 761 741 692 (%) TensileYield Str - MD 9.1 7.9 8 9.7 10.1 (Mpa) Tensile Yield Str - TD 8.9 7.67.7 9.9 9.2 (Mpa) Tensile Elong at Yield - 13 10 16 15 16 MD (%) TensileElong at Yield - 14 10 15 14 12 TD (%) Film Opticals Gloss at 45° 7283.8 67 39 84 Haze (%) 5.8 2.9 6.8 16.2 3.3 Cold Seal Properties S.I.T.@ 8.8 N Seal 98.2 93.5 89.75 102.8 102.4 Strength (° C.) Max Force (N)23.7 24.4 24.70 20.6 23.4 Temp. @ Max Force (° C.) 160 160 155 140 120Hot Tack Properties Tack Onset @ 1.0 N (° C.) - 95.4 87 78 101.2 98.6 2mil film Max Hottack Strength (N) - 4.4 5.1 3.5 5.3 5.7 2 mil filmTemperature - Max. 115 105 120 120 120 Hottack (° C.) - 2 mil film AHTW(Newtons · ° C.) 111 151 114 103 103.5 OTR (cm³ per 100 Comparative 8Comparative 9 Film Physical Properties Thickness Profile Ave 1 1 (mil)Film Toughness Dart Impact (g/mil) 214 156 Slow Puncture - Lube/Tef 7325 (J/mm) ASTM Puncture (J/mm) 78.5 78 Film Tear Resistance Tear - MD(g/mil) 384 295 Tear - TD (g/mil) 616 640 Film Stiffness 1% SecModulus - MD 193 243 (Mpa) 1% Sec Modulus - TD 197 252 (Mpa) 2% SecModulus - MD 176 213 (Mpa) 2% Sec Modulus - TD 179 220 (Mpa) FilmTensile Strength Tensile Break Str - MD 52.6 38.4 (Mpa) Tensile BreakStr - TD 42.8 35.8 (Mpa) Elongation at Break - MD 608 707 (%) Elongationat Break - TD 767 729 (%) Tensile Yield Str - MD 10.4 12.7 (Mpa) TensileYield Str - TD 10.4 13.2 (Mpa) Tensile Elong at Yield - 10.2 10.5 MD (%)Tensile Elong at Yield - 10.7 13.2 TD (%) Film Opticals Gloss at 45°61.7 56 Haze (%) 11.8 14.0 Cold Seal Properties S.I.T. @ 8.8 N Seal107.5 116.0 Strength (° C.) Max Force (N) 26.5 31.9 Temp. @ Max Force (°C.) 150 180 Hot Tack Properties Tack Onset @ 1.0 N (° C.) - 98.75 106.42 mil film Max Hottack Strength (N) - 4.16 4.3 2 mil film Temperature -Max. 120 140 Hottack (° C.) - 2 mil film AHTW (Newtons · ° C.) 139.128.4 OTR (cm³ per 100 inch²) 650.8 382.4

The data provided in Table 5 together with the data in FIGS. 4-8demonstrate that the inventive polyethylene compositions can be madeinto film having a good balance of film properties, including goodstiffness, good oxygen transmission rates and good sealing properties.For example, and with reference to FIGS. 4-8, the films made from theinventive polyethylene compositions have good hot tack and cold sealperformance.

Without wishing to be bound by theory, in the hot tack (or cold seal)profile (seal temperature vs. seal force), good hot tack (or cold seal)performance is indicated by an early (or low) hot tack (or cold seal)initiation temperature, then a relatively high sealing force over a widerange of hot tack seal temperatures. See for example the shape thecurves in FIGS. 4 and 5 for Inventive Examples 1 and 2, relative toComparative Examples 1-7. The shape of the hot tack curves for InventiveExamples 1 and 2, are particularly good and have an early hot tack sealinitiation temperature combined by a high sealing force over a widerange of hot tack seal temperatures. In an effort to provide a morequantitatively measurement of this improved hot tack sealingperformance, a new parameter, the “area of the hot-tack (strength)window” (the “area of hot tack window” or the “AHTW”) has been definedherein. The AHTW is simply an estimate of the area under the hot tackcurve from the hot-tack on-set temperature to the temperatureimmediately prior to the melting of the specimen. As shown in FIG. 4,the temperature prior to the melting of the specimen was typically at130° C., but not necessarily at 130° C. As shown in Table 5 and in FIG.4, the Inventive Examples 1 and 2 each have an AHTW of greater than 160Newtons·° C., whereas each of the Comparative Examples, 1-7, have anAHTW of less than 160 Newtons-° C.

Good cold seal properties are evidenced by the curves given in FIG. 5for the Inventive Examples 1 and 2. For comparison, the cold sealproperties of Comparative Examples 1-7 are also shown in FIG. 5. FromFIG. 5, a person skilled in the art will recognize that the InventiveExamples 1 and 2 each have an early cold seal initiation temperature incombination with a relatively high seal force over a wide range of coldseal temperatures. In contrast, the Comparative Examples, 1-7 have alater cold seal initiation temperature, with a narrower range of coldseal temperatures over which a relatively high seal force occurs.

FIG. 6 shows that the Inventive Examples 1 and 2, have a better balanceof AHTW and stiffness (as determined by the machine direction (MD)secant modulus at 1% strain) than do the Comparative Examples 2-9.Indeed, FIG. 6, which plots the AHTW (in Newtonso·° C.) values (they-axis) against the machine direction (MD) secant modulus at 1% strain(in MPa) values (the x-axis), along with plot of the equation:AHTW=−2.0981 (machine direction (MD) 1% secant modulus)+564.28, showsthat the Inventive Examples 1 and 2 satisfy the condition: AHTW>−2.0981(machine direction (MD) 1% secant modulus)+564.28, whereas theComparative Examples 2-9 do not.

FIG. 7, shows that the Inventive Examples 1 and 2, have a better balanceof SIT and stiffness (as determined by the machine direction (MD) secantmodulus at 1% strain) than do the Comparative Examples 2-9. FIG. 7,which plots the SIT (in ° C.) values (the y-axis) against the machinedirection (MD) secant modulus at 1% strain (in MPa) values (the x-axis),along with plot of the equation: SIT=0.366 (machine direction (MD) 1%secant modulus)+22.509, shows that the Inventive Examples 1 and 2satisfy the condition: SIT<0.366 (machine direction (MD) 1% secantmodulus)+22.509, whereas the Comparative Examples 2-9 do not.

FIG. 8, shows that the Inventive Examples 1 and 2, have a better balanceof OTR and stiffness (as determined by the machine direction (MD) secantmodulus at 1% strain) than do the Comparative Examples 2-9. FIG. 8,which plots the OTR (in cm³ per 100 inch²) values (the y-axis) againstthe machine direction (MD) secant modulus at 1% strain (in MPa) values(the x-axis), along with plot of the equation: OTR=−5.4297 (machinedirection (MD) 1% secant modulus)+1767.8, shows that the InventiveExamples 1 and 2 satisfy the condition: OTR>−5.4297 (machine direction(MD) 1% secant modulus)+1767.8, whereas the Comparative Examples 2-9 donot.

Non-limiting embodiments of the present disclosure include thefollowing:

Embodiment A

A polyethylene composition comprising:

from 5 to 80 wt % of a first polyethylene which is an ethylenecopolymer, the first polyethylene having a weight average molecularweight M_(w) of from 70,000 to 250,000, a molecular weight distributionM_(w)/M_(n) of <2.3 and from 5 to 100 short chain branches per thousandcarbon atoms;

-   -   from 5 to 80 wt % of a second polyethylene which is an ethylene        copolymer or an ethylene homopolymer, the second polyethylene        having a weight average molecular weight M_(w) of from 15,000 to        100,000, a molecular weight distribution M_(w)/M_(n) of <2.3 and        from 0 to 20 short chain branches per thousand carbon atoms; and

from 5 to 80 wt % of a third polyethylene which is an ethylene copolymeror an ethylene homopolymer, the third polyethylene having a weightaverage molecular weight M_(w) of from 70,000 to 250,000, a molecularweight distribution M_(w)/M_(n) of ≥2.3 and from 0 to 50 short chainbranches per thousand carbon atoms; wherein

the number of short chain branches per thousand carbon atoms in firstpolyethylene (SCB_(PE-1)) is greater than the number of short chainbranches per thousand carbon atoms in the second polyethylene(SCB_(PE-2)) and the third polyethylene (SCB_(PE-3));

the number of short chain branches per thousand carbon atoms in thethird polyethylene (SCB_(PE-3)) is greater than the number of shortchain branches per thousand carbon atoms in the second polyethylene(SCB_(PE-2)); and

the weight average molecular weight of the second polyethylene is lessthan the weight average molecular weight of the first polyethylene andthe third polyethylene; wherein,

the polyethylene composition has a density of ≤0.939 g/cm³, a melt indexI₂ of from 0.1 to 10 dg/min, a melt flow ratio, I₂₁/I₂ of ≤40 and has asoluble fraction in a crystallization elution fractionation (CEF)analysis of at least 10 weight percent.

Embodiment B

The polyethylene composition of Embodiment A wherein the polyethylenecomposition has a unimodal profile in a gel permeation chromatograph(GPC).

Embodiment C

The polyethylene composition of Embodiment A or B wherein thepolyethylene composition has a soluble fraction in a crystallizationelution fractionation (CEF) analysis of at least 15 weight percent.

Embodiment D

The polyethylene composition of Embodiment A, B or C wherein thepolyethylene composition has a melting peak temperature in adifferential scanning calorimetry (DSC) analysis at above 125° C.

Embodiment E

The polyethylene composition of Embodiment A, B, C or D wherein thefirst polyethylene has from 30 to 75 short chain branches per thousandcarbon atoms.

Embodiment F

The polyethylene composition of Embodiment A, B, C, D or E wherein thesecond polyethylene is an ethylene homopolymer.

Embodiment G

The polyethylene composition of Embodiment A, B, C, D, E or F whereinthe third polyethylene is an ethylene copolymer and has from 5 to 30short chain branches per thousand carbon atoms.

Embodiment H

The polyethylene composition of Embodiment A, B, C, D, E, F or G whereinthe first polyethylene has a weight average molecular weight, M_(w) offrom 75,000 to 200,000.

Embodiment I

The polyethylene composition of Embodiment A, B, C, D, E, F, G or Hwherein the second polyethylene has a weight average molecular weight,M_(w) of from 25,000 to 75,000.

Embodiment J

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H or Iwherein the third polyethylene has a weight average molecular weight,M_(w) of from 80,000 to 200,000.

Embodiment K

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I orJ wherein the first polyethylene has a density of from 0.855 to 0.910g/cm³.

Embodiment L

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, Jor K wherein the second polyethylene is an ethylene homopolymer having adensity of from 0.940 to 0.980 g/cm³.

Embodiment M

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K or L wherein the third polyethylene is an ethylene copolymer having adensity of from 0.880 to 0.936 g/cm³.

Embodiment N

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L or M wherein the first polyethylene is present in from 5 to 50 wt%.

Embodiment O

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M or N wherein the second polyethylene is present in from 5 to 60wt %.

Embodiment P

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N or O wherein the third polyethylene is present in from 15 to85 wt %.

Embodiment Q

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L or M wherein the first polyethylene is present in from 10 to 40 wt%.

Embodiment R

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M or Q wherein the second polyethylene is present in from 15 to 45wt %.

Embodiment S

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, Q or R wherein the third polyethylene is present in from 20 to80 wt %.

Embodiment T

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R or S wherein the first polyethylene has a CDBI₅₀of at least 75 wt %.

Embodiment U

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S or T wherein the third polyethylene is acopolymer with a CDBI₅₀ of less than 75 wt %.

Embodiment V

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T or U wherein the first polyethylene is ahomogeneously branched ethylene copolymer.

Embodiment W

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U or V wherein the third polyethylene is aheterogeneously branched ethylene copolymer.

Embodiment X

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V or W wherein the first polyethyleneis a made with a single site catalyst.

Embodiment Y

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W or X wherein the secondpolyethylene is made with a single site catalyst.

Embodiment Z

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X or Y wherein the thirdpolyethylene is made with a Ziegler-Natta catalyst.

Embodiment AA

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y or Z wherein thepolyethylene composition has a molecular weight distribution M_(w)/M_(n)of from 2.1 to 5.5.

Embodiment BB

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y or Z wherein thepolyethylene composition has a molecular weight distribution M_(w)/M_(n)of from 2.1 to 4.5.

Embodiment CC

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA or BB wherein thepolyethylene composition has a density of <0.935 g/cm³.

Embodiment DD

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA or BB wherein thepolyethylene composition has a density of from 0.880 to 0.932 g/cm³.

Embodiment EE

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA, BB, CC or DD whereinthe polyethylene composition has a melt index, I₂ of from 0.1 to 3.0dg/min.

Embodiment FF

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA, BB, CC, DD or EE orwherein the polyethylene composition has a M_(Z)/M_(W) of less than 3.0.

Embodiment GG

The polyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J,K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA, BB, CC, DD, EE or FFwherein the polyethylene composition has a melt index ratio, I₂₁/I₂ offrom 20 to 40.

Embodiment HH

A film layer having a thickness of from 0.5 to 10 mil, comprising thepolyethylene composition of Embodiment A, B, C, D, E, F, G, H, I, J, K,L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA, BB, CC, DD, EE, FF orGG.

Embodiment II

The film layer of Embodiment HH wherein the film layer has a machinedirection (MD) 1% secant modulus of ≥190 MPa when measured at a filmthickness of about 1 mil.

Embodiment JJ

The film layer of Embodiment HH or II wherein the film layer has a sealinitiation temperature (SIT) of ≤100° C. when measured at a filmthickness of about 2 mil.

Embodiment KK

The film layer of Embodiment HH, II or JJ wherein the film layer has anarea of hot tack window (AHTW) of ≥160 Newtons·° C. when measured at afilm thickness of about 2 mil.

Embodiment LL

The film layer of Embodiment HH, II, JJ or KK wherein the film layer hasan oxygen transmission rate (OTR) of ≥650 cm³ per 100 inch² whenmeasured at a film thickness of about 1 mil.

Embodiment MM

The film layer of Embodiment HH wherein the film layer has a machinedirection (MD) 1% secant modulus of ≥190 MPa when measured at a filmthickness of about 1 mil, a seal initiation temperature (SIT) of ≤100°C. when measured at a film thickness of about 2 mil, an area of hot tackwindow (AHTW) of >160 Newtons·° C. when measured at a film thickness ofabout 2 mil, and an oxygen transmission rate (OTR) of ≥650 cm³ per 100inch² when measured at a film thickness of about 1 mil.

Embodiment NN

A film layer having a thickness of from 0.5 to 10 mil, wherein the filmlayer has a machine direction (MD) 1% secant modulus of ≤190 MPa whenmeasured at a film thickness of about 1 mil and a seal initiationtemperature (SIT) of ≤100° C. when measured at a film thickness of about2 mil.

Embodiment OO

A film layer having a thickness of from 0.5 to 10 mil, wherein the filmlayer has a has a machine direction (MD) 1% secant modulus of −190 MPawhen measured at a film thickness of about 1 mil and an area of hot tackwindow (AHTW) of ≤160 Newtons·° C. when measured at a film thickness ofabout 2 mil.

Embodiment PP

A film layer having a thickness of from 0.5 to 10 mil, wherein the filmlayer has a has a machine direction (MD) 1% secant modulus of −190 MPawhen measured at a film thickness of about 1 mil and an oxygentransmission rate (OTR) of ≥650 cm³ per 100 inch² when measured at afilm thickness of about 1 mil.

Embodiment QQ

A film layer having a thickness of from 0.5 to 10 mil, wherein the filmlayer has a has a machine direction (MD) 1% secant modulus of −190 MPawhen measured at a film thickness of about 1 mil, an oxygen transmissionrate (OTR) of ≥650 cm³ per 100 inch² when measured at a film thicknessof about 1 mil, a seal initiation temperature (SIT) of ≤100° C. whenmeasured at a film thickness of about 2 mil, and an area of hot tackwindow (AHTW) of ≥160 Newtons·° C. when measured at a film thickness ofabout 2 mil.

Embodiment RR

Film comprising the polyethylene composition of Embodiment A, B, C, D,E, F, G, H, I, J, K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA,BB, CC, DD, EE, FF or GG, the film satisfying the followingrelationship:

area of hot tack window (AHTW)>−2.0981 (machine direction (MD) 1% secantmodulus)+564.28;

-   -   wherein the AHTW is measured at a film thickness of about 2 mil,        and the machine direction (MD) 1% secant modulus is measured at        a film thickness of about 1 mil.

Embodiment SS

Film comprising the polyethylene composition of Embodiment A, B, C, D,E, F, G, H, I, J, K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA,BB, CC, DD, EE, FF or GG, the film satisfying the followingrelationship:

oxygen transmission rate (OTR)>−5.4297 (machine direction (MD) 1% secantmodulus)+1767.8;

wherein the OTR is measured at a film thickness of about 1 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil.

Embodiment TT

Film comprising the polyethylene composition of Embodiment A, B, C, D,E, F, G, H, I, J, K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA,BB, CC, DD, EE, FF or GG, the film satisfying the followingrelationship:

seal initiation temperature (SIT)<0.366 (machine direction (MD) 1%secant modulus)+22.509;

wherein the SIT is measured at a film thickness of about 2 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil.

Embodiment UU

Film comprising the polyethylene composition of Embodiment A, B, C, D,E, F, G, H, I, J, K, L, M, N, O, P, Q, R, S, T, U, V, W, X, Y, Z, AA,BB, CC, DD, EE, FF or GG, the film satisfying the followingrelationships: i) area of hot tack window (AHTW)>−2.0981 (machinedirection (MD) 1% secant modulus)+564.28;

wherein the AHTW is measured at a film thickness of about 2 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil;

ii) oxygen transmission rate (OTR)>−5.4297 (machine direction (MD) 1%secant modulus)+1767.8;

wherein the OTR is measured at a film thickness of about 1 mil, and themachine direction (MD) 1% secant modulus is measured at a film thicknessof about 1 mil; and

iii) seal initiation temperature (SIT)<0.366 (machine direction (MD) 1%secant modulus)+22.509;

-   -   wherein the SIT is measured at a film thickness of about 2 mil,        and the machine direction (MD) 1% secant modulus is measured at        a film thickness of about

What is claimed is:
 1. A polyethylene composition comprising: from 5 to80 wt % of a first polyethylene which is an ethylene copolymer, thefirst polyethylene having a weight average molecular weight M_(w) offrom 70,000 to 250,000, a molecular weight distribution M_(w)/M_(n) of<2.3 and from 5 to 100 short chain branches per thousand carbon atoms;from 5 to 80 wt % of a second polyethylene which is an ethylenecopolymer or an ethylene homopolymer, the second polyethylene having aweight average molecular weight M_(w) of from 15,000 to 100,000, amolecular weight distribution M_(w)/M_(n) of <2.3 and from 0 to 20 shortchain branches per thousand carbon atoms; and from 5 to 80 wt % of athird polyethylene which is an ethylene copolymer or an ethylenehomopolymer, the third polyethylene having a weight average molecularweight M_(w) of from 70,000 to 250,000, a molecular weight distributionM_(w)/M_(n) of ≥2.3 and from 0 to 50 short chain branches per thousandcarbon atoms; wherein the number of short chain branches per thousandcarbon atoms in the first polyethylene (SCB_(PE-1)) is greater than thenumber of short chain branches per thousand carbon atoms in the secondpolyethylene (SCB_(PE-2)) and the third polyethylene (SCB_(PE-3)); thenumber of short chain branches per thousand carbon atoms in the thirdpolyethylene (SCB_(PE-3)) is greater than the number of short chainbranches per thousand carbon atoms in the second polyethylene(SCB_(PE-2)); and the weight average molecular weight of the secondpolyethylene is less than the weight average molecular weight of thefirst polyethylene and the third polyethylene; wherein, the polyethylenecomposition has a density of ≤0.939 g/cm³, a melt index I₂ of from 0.1to 10 dg/min, a melt flow ratio, I₂₁/I₂ of ≤40 and has a solublefraction in a crystallization elution fractionation (CEF) analysis of atleast 10 weight percent.
 2. The polyethylene composition of claim 1wherein the polyethylene composition has a unimodal profile in a gelpermeation chromatograph (GPC).
 3. The polyethylene composition of claim1 wherein the polyethylene composition has a soluble fraction in acrystallization elution fractionation (CEF) analysis of at least 15weight percent.
 4. The polyethylene composition of claim 1 wherein thepolyethylene composition has a melting peak temperature in adifferential scanning calorimetry (DSC) analysis at above 125° C.
 5. Thepolyethylene composition of claim 1 wherein the first polyethylene hasfrom 30 to 75 short chain branches per thousand carbon atoms.
 6. Thepolyethylene composition of claim 1 wherein the second polyethylene isan ethylene homopolymer.
 7. The polyethylene composition of claim 1wherein the third polyethylene is an ethylene copolymer and has from 5to 30 short chain branches per thousand carbon atoms.
 8. Thepolyethylene composition of claim 1 wherein the first polyethylene has aweight average molecular weight, M_(w) of from 75,000 to 200,000.
 9. Thepolyethylene composition of claim 1 wherein the second polyethylene hasa weight average molecular weight, M_(w) of from 25,000 to 75,000. 10.The polyethylene composition of claim 1 wherein the third polyethylenehas a weight average molecular weight, M_(w) of from 80,000 to 200,000.11. The polyethylene composition of claim 1 wherein the firstpolyethylene has a density of from 0.855 to 0.910 g/cm³.
 12. Thepolyethylene composition of claim 1 wherein the second polyethylene isan ethylene homopolymer having a density of from 0.940 to 0.980 g/cm³.13. The polyethylene composition of claim 1 wherein the thirdpolyethylene is an ethylene copolymer having a density of from 0.880 to0.936 g/cm³.
 14. The polyethylene composition of claim 1 wherein thefirst polyethylene is present in from 5 to 50 wt. %.
 15. Thepolyethylene composition of claim 1 wherein the second polyethylene ispresent in from 5 to 60 wt. %.
 16. The polyethylene composition of claim1 wherein the third polyethylene is present in from 15 to 85 wt. %. 17.The polyethylene composition of claim 1 wherein the first polyethyleneis present in from 10 to 40 wt. %.
 18. The polyethylene composition ofclaim 1 wherein the second polyethylene is present in from 15 to 45 wt.%.
 19. The polyethylene composition of claim 1 wherein the thirdpolyethylene is present in from 20 to 80 wt. %.
 20. The polyethylenecomposition of claim 1 wherein the first polyethylene has a CDBI₅₀₀ ofat least 75 wt. %.
 21. The polyethylene composition of claim 1 whereinthe third polyethylene is a copolymer with a CDBI₅₀ of less than 75 wt.%.
 22. The polyethylene composition of claim 1 wherein the firstpolyethylene is a homogeneously branched ethylene copolymer.
 23. Thepolyethylene composition of claim 1 wherein the third polyethylene is aheterogeneously branched ethylene copolymer.
 24. The polyethylenecomposition of claim 1 wherein the first polyethylene is a made with asingle site catalyst.
 25. The polyethylene composition of claim 1wherein the second polyethylene is made with a single site catalyst. 26.The polyethylene composition of claim 1 wherein the third polyethyleneis made with a Ziegler-Natta catalyst.
 27. The polyethylene compositionof claim 1 wherein the polyethylene composition has a molecular weightdistribution M_(w)/M_(n) of from 2.1 to 5.5.
 28. The polyethylenecomposition of claim 1 wherein the polyethylene composition has amolecular weight distribution M_(w)/M_(n) of from 2.1 to 4.5.
 29. Thepolyethylene composition of claim 1 wherein the polyethylene compositionhas a density of <0.935 g/cm³.
 30. The polyethylene composition of claim1 wherein the polyethylene composition has a density of from 0.880 to0.932 g/cm³.
 31. The polyethylene composition of claim 1 wherein thepolyethylene composition has a melt index, I₂ of from 0.1 to 3.0 dg/min.32. The polyethylene composition of claim 1 wherein the polyethylenecomposition has a M_(Z)/M_(W) of less than 3.0.
 33. The polyethylenecomposition of claim 1 wherein the polyethylene composition has a meltindex ratio, I₂₁/I₂ of from 20 to
 40. 34. A film layer having athickness of from 0.5 to 10 mil, comprising the polyethylene compositionof claim
 1. 35. The film layer of claim 34 wherein the film layer has amachine direction (MD) 1% secant modulus of 190 MPa when measured at afilm thickness of about 1 mil.
 36. The film layer of claim 34 whereinthe film layer has a seal initiation temperature (SIT) of ≤100° C. whenmeasured at a film thickness of about 2 mil.
 37. The film layer of claim34 wherein the film layer has an area of hot tack window (AHTW) of ≥160Newtons·° C. when measured at a film thickness of about 2 mil.
 38. Thefilm layer of claim 34 wherein the film layer has an oxygen transmissionrate (OTR) of <650 cm³ per 100 inch² when measured at a film thicknessof about 1 mil.
 39. The film layer of claim 34 wherein the film layerhas a machine direction (MD) 1% secant modulus of ≥190 MPa when measuredat a film thickness of about 1 mil, a seal initiation temperature (SIT)of <100° C. when measured at a film thickness of about 2 mil, an area ofhot tack window (AHTW) of ≥160 Newtons-° C. when measured at a filmthickness of about 2 mil, and an oxygen transmission rate (OTR) of ≥650cm³ per 100 inch² when measured at a film thickness of about 1 mil. 40.A film layer having a thickness of from 0.5 to 10 mil, wherein the filmlayer has a machine direction (MD) 1% secant modulus of ≥190 MPa whenmeasured at a film thickness of about 1 mil and a seal initiationtemperature (SIT) of <100° C. when measured at a film thickness of about2 mil.
 41. A film layer having a thickness of from 0.5 to 10 mil,wherein the film layer has a has a machine direction (MD) 1% secantmodulus of ≥190 MPa when measured at a film thickness of about 1 mil andan area of hot tack window (AHTW) of ≥160 Newtons-° C. when measured ata film thickness of about 2 mil.
 42. A film layer having a thickness offrom 0.5 to 10 mil, wherein the film layer has a has a machine direction(MD) 1% secant modulus of ≥190 MPa when measured at a film thickness ofabout 1 mil and an oxygen transmission rate (OTR) of ≥650 cm³ per 100inch² when measured at a film thickness of about 1 mil.
 43. A film layerhaving a thickness of from 0.5 to 10 mil, wherein the film layer has ahas a machine direction (MD) 1% secant modulus of ≥190 MPa when measuredat a film thickness of about 1 mil, an oxygen transmission rate (OTR) of≥650 cm³ per 100 inch² when measured at a film thickness of about 1 mil,a seal initiation temperature (SIT) of <100° C. when measured at a filmthickness of about 2 mil, and an area of hot tack window (AHTW) of ≥160Newtons·° C. when measured at a film thickness of about 2 mil.
 44. Filmcomprising the polyethylene composition of claim 1, the film satisfyingthe following relationship: area of hot tack window (AHTW)>−2.0981(machine direction (MD) 1% secant modulus)+564.28; wherein the AHTW ismeasured at a film thickness of about 2 mil, and the machine direction(MD) 1% secant modulus is measured at a film thickness of about 1 mil.45. Film comprising the polyethylene composition of claim 1, the filmsatisfying the following relationship: oxygen transmission rate(OTR)>−5.4297 (machine direction (MD) 1% secant modulus)+1767.8; whereinthe OTR is measured at a film thickness of about 1 mil, and the machinedirection (MD) 1% secant modulus is measured at a film thickness ofabout 1 mil.
 46. Film comprising the polyethylene composition of claim1, the film satisfying the following relationship: seal initiationtemperature (SIT)<0.366 (machine direction (MD) 1% secantmodulus)+22.509; wherein the SIT is measured at a film thickness ofabout 2 mil, and the machine direction (MD) 1% secant modulus ismeasured at a film thickness of about 1 mil.
 47. Film comprising thepolyethylene composition of claim 1, the film satisfying the followingrelationships: i) area of hot tack window (AHTW)>−2.0981 (machinedirection (MD) 1% secant modulus)+564.28; wherein the AHTW is measuredat a film thickness of about 2 mil, and the machine direction (MD) 1%secant modulus is measured at a film thickness of about 1 mil; ii)oxygen transmission rate (OTR)>−5.4297 (machine direction (MD) 1% secantmodulus)+1767.8; wherein the OTR is measured at a film thickness ofabout 1 mil, and the machine direction (MD) 1% secant modulus ismeasured at a film thickness of about 1 mil; and iii) seal initiationtemperature (SIT)<0.366 (machine direction (MD) 1% secantmodulus)+22.509; wherein the SIT is measured at a film thickness ofabout 2 mil, and the machine direction (MD) 1% secant modulus ismeasured at a film thickness of about 1 mil.